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Faget, Maxime A

Faget

American Chief Designer of American manned spacecraft. Designed Mercury, Apollo, and Shuttle spacecraft.

Born: 1921-08-26. Died: 2004-10-09. Birth Place: Stann Creek.

Shortly described as an egocentric genius, Napoleonic in stature (5'6") and drive, Faget was the "Chief Designer" of America's manned space program during the race to the moon.

Max was a wrestler while at Louisiana State University. After graduating in 1943, he volunteered for the submarine service. Surviving the war, he joined the staff at Langley Aeronautical Laboratory in 1946. He soon became head of the performance aerodynamics branch of the pilotless aircraft research division. There he conducted research on the blunt heat shield concept that would later be applied to the Mercury spacecraft. In 1958 he joined the Space Task Group in NASA (forerunner of the Johnson Space Center), and he became its Assistant Director for Engineering and Development in 1962 and later its Director.

When the country needed a crash program to put a man into space or send a man to the moon, Faget had very definite ideas on the simplified re-entry capsule configuration needed to do the job in the shortest time necessary. He also had very definite ideas on everything else - subsystems, landing techniques, avionics. Faget's concepts were brought to life by Caldwell Johnson, a high school graduate who was Faget's master assistant of design and layout. Although NASA went through a bidding process for Mercury, Apollo, and the Space Shuttle, the contractors that followed Max' vision won; those who thought they had a better idea, lost.

While Faget virtually dictated the design of Mercury, Gemini, and Apollo, he lost the internal battle for his favored stub-winged, low cross-range design for the Space Shuttle. He retired from NASA in 1981 and became an executive for Eagle Engineering, Inc. In 1982 he was one of the founders of Space Industries, Inc. and became its president and chief executive officer.

Faget's numerous accomplishments include patents on the escape tower concept used on the Mercury, Apollo, and Soyuz spacecraft; the Mercury capsule, and the standard Mach number indicator. He received numerous honors and awards, including the Arthur S. Flemming Award, the NASA Medal for Outstanding Leadership, and honorary doctorates of engineering degrees from the University of Pittsburgh and Louisiana State University. He was inducted into the National Space Hall of Fame in 1969 and the National Inventors Hall of Fame in 2003. Faget was the first recipient of the Rotary National Award for Space Achievement in 1987.

Faget's wife, Nancy passed away in 1994. At the time of his death he was survived by four children: Ann, Carol, Guy, and Nanette; a daughter in law, two sons in law and 10 grandchildren.

Country: Belize, USA. Agency: USN. Bibliography: 4472, 535, 5366.

1921 August 26 - .

• Birth of Maxime A Faget - . Nation: Belize, USA. Related Persons: Faget. American Chief Designer of American manned spacecraft. Designed Mercury, Apollo, and Shuttle spacecraft..

1957 November - .

• Faget presentation on manned orbital flight. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  A presentation on manned orbital flight was made by Maxime A. Faget. The concept included the use of existing ballistic missiles for propulsion, solid-fuel retrorockets for reentry initiation, and a nonlifting ballistic shape for the reentering capsule. This concept was considered to be the quickest and safest approach for initial manned flights into orbit.

1957 December 1 - .

• Mercury ballistic shape proposed. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury. Maxime Faget of NACA Langley proposed ballistic shape of Mercury capsule, while A. Eggers of Ames and E. S. Love and J. V. Becker of Langley proposed glider configurations of manned spacecraft later incorporated in Dyna-Soar and Apollo studies..

1958 January 16 - . Launch Vehicle: Little Joe.

• Little Joe launch vehicle conceived. - . Nation: USA. Related Persons: Faget.
  Paul E. Purser and Maxime A. Faget conceived of a solid-fuel launch vehicle design for the research and development phase of a manned satellite vehicle project. This launch vehicle was later designated Little Joe. When Project Mecury began in October 1958, the purposeof the Little Joe phase was to propel a full-scale, full-weight developmental version of the manned spacecraft to some of the flight conditions that would be encountered during exit from the atmosphere on an orbital mission. Also, Little Joe tests were used to perfect the escape maneuver in the event of an aborted mission.

1958 January 29-31 - .

• Conference reviews concepts for manned orbital vehicles. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury, Project 7969.
  A conference was held at Wright-Patterson Air Force Base, Ohio, to review concepts for manned orbital vehicles. The NACA informally presented two concepts then under study at Langley Aeronautical Laboratory: the one proposed by Maxime A. Faget involved a ballistic, high-drag capsule with heat shield on which the pilot lies prone during reentry, with reentry being accomplished by reverse thrust at the apogee of the elliptical orbit involving a deceleration load of about 8g, and proceeding to impact by a parachute landing; the other Langley proposal called for the development of a triangular planform vehicle with a flat bottom having some lift during reentry. At this same meeting there were several Air Force contractor presentations. These were as follows: Northrop, boost-glide buildup to orbital speed; Martin, zero-lift vehicle launched by a Titan with controlled flight estimated to be possible by mid-1961; McDonnell, ballistic vehicle resembling Faget's proposal, weighing 2,400 pounds and launched by an Atlas with a Polaris second stage; Lockheed, a 20 degree semiapex angle cone with a hemispherical tip of 1-foot radius, pilot in sitting position facing rearward, to be launched by an Atlas-Hustler combination; Convair reviewed a previous proposal for a large-scale manned space station, but stated a minimum vehicle - a 1,000-pound sphere - could be launched by an Atlas within a year; Aeronutronics, cone-shaped vehicle with spherical tip of 1-foot radius, with man enclosed in sphere inside vehicle and rotated to line the pilot up with accelerations, and launched by one of several two-stage vehicles; Republic, the Ferri sled vehicle, a 4,000 pound, triangular plan with a two-foot diameter tube running continuous around the leading and trailing edge and serving as a fuel tank for final-stage, solid-propellant rockets located in each wing tip, with a man in small compartment on top side, and with a heat-transfer ring in the front of the nose for a glide reentry of 3,600 miles per hour with pilot ejecting from capsule and parachuting down, and the launch vehicle comprising three stages (also see July 31, 1958 entry); AVCO, a 1,500-pound vehicle sphere launched by a Titan, equipped with a stainless-steel-cloth parachute whose diameter would be controlled by compessed air bellows and which would orient the vehicle in orbit, provide deceleration for reentry, and control drag during reentry; Bell, reviewed proposals for boost-glide vehicles, but considered briefly a minimum vehicle, spherical in shape, weighing about 3,000 pounds; Goodyear, a spherical vehicle with a rearward facing tail cone and ablative surface, with flaps deflected from the cone during reentry for increased drag and control, and launched by an Atlas or a Titan plus a Vanguard second stage; North American, extend the X-15 program by using the X-15 with a three-stage launch vehicle to achieve a single orbit with an apogee of 400,000 feet and a perigee of 250,000, range about 500 to 600 miles and landing in the Gulf of Mexico, and the pilot ejecting and landing by parachute with the aircraft being lost.

1958 March 18-20 - .

• NACA Conference on High-Speed Aerodynamics - . Nation: USA. Related Persons: Faget. Spacecraft: Dynasoar, Mercury.
  An 'NACA Conference on High-Speed Aerodynamics' was held at the Ames Aeronautical Laboratory, Moffett Field, California, to acquaint the military services and industrial contractors interested in aerospace projects with the results of recent research conducted by the NACA laboratories on the subject of space flight. The conference was attended by more than 500 representatives from the NACA, industry, the military services, and other appropriate government agencies. Some 46 technical papers were presented by NACA personnel, and included specific proposals for manned space flight vehicle projects. One of these was presented by Maxime A. Faget. Other papers within the category of manned orbital satellites included: 'Preliminary Studies of Manned Satellites, Wingless Configuration, Lifting Body' by Thomas J. Wong and others; 'Preliminary Studies of Manned Satellites, Winged Configurations' by John V. Becker; 'Preliminary Aerodynamic Data Pertinent to Manned Satellite Reentry Configurations' by Jim A. Penland and William O. Armstrong; and 'Structural Design Considerations for Boost-Glide and Orbital Reentry Vehicles' by William A. Brooks and others.

1958 March 18 - .

• Preliminary Studies of Manned Satellites, Wingless Configuration, Non-Lifting - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  An NACA report was published entitled, 'Preliminary Studies of Manned Satellites, Wingless Configuration, Non-Lifting,' by Maxime A. Faget, Benjamine Garland, and James J. Buglia. Later this document became the basic working paper for the Project Mercury development program, and was reissued as NASA Technical Note D-1254, March 1962.

1958 April - .

• Faget conceived contour couch to withstand the high g-loads. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  Maxime A. Faget and associates conceived the idea of using a contour couch to withstand the high g-loads attendant to acceleration and reentry forces of manned space flight. Fabrication of test-model contour couches was started in the Langley shops in May 1958, and the concept was proved feasible on July 30 of that same year.

1958 June - .

• Preliminary specifications of the first manned satellite vehicle. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  Preliminary specifications of the first manned satellite vehicle were drafted by Langley Aeronautical Laboratory personnel under the supervision of Maxime Faget and Charles W. Mathews. After a number of revisions and additions, these specifications were used for the Project Mercury spacecraft contract with McDonnell Aircraft Corporation. A working group of representatives from the Langley Aeronautical Laboratory and the Lewis Flight Propulsion Laboratory was formed for the purpose of outlining a manned satellite program.

1958 June 5 - .

• Advanced Research Projects Agency manned space project. - . Nation: USA. Related Persons: Faget. Spacecraft Bus: Mercury. Spacecraft: Mercury, Man-In-Space-Soonest, Project 7969.
  After serving as a liaison officer of NACA and as a participating member of an Advanced Research Projects Agency panel, Maxime A. Faget reported to Dr. Hugh Dryden on resulting studies and attending recommendations on the subject of manned space flight. He stated that the Advanced Research Projects Agency panel was quite aware that the responsibility for such a program might be placed with the soon-to-be-created civilian space agency, although they recommended program management be placed with the Air Force under executive control of NACA and the Advanced Research Projects Agency. The panel also recommended that the program start immediately even though the specific manager was, as yet, unassigned. Several of the proposals put forth by the panel on the proposed development were rather similar to the subsequent evolvement. The system suggested by the Advanced Research Projects Agency was to be based on the use of the Atlas launch vehicle with the Atlas-Sentry system serving as backup; retrorockets were to be used to initiate the return from orbit; the spacecraft was to be nonlifting, ballistic type, and the crew was to be selected from qualified volunteers in the Army, Navy, and Air Force.

1958 July - .

• Mercury escape rocket conceived. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury, Mercury Escape Tower. The initial concept of the use of a tractor rocket for an escape device was suggested by Maxime A. Faget. The idea was developed into the Mercury escape rocket..

1958 July 30 - .

• Test subject withstood a 20g load on the centrifuge using Langley contour couch. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  By using the development model of the Mercury contour couch designed by Maxime A. Faget and associates, Carter C. Collins withstood a 20g load on the centrifuge at Johnsville, Pennsylvania. This test proved that the reentry accelerations of manned space flight could be withstood.

1958 September 24-October 1 - .

• Basic plan for a manned satellite program. - . Nation: USA. Related Persons: Faget, Gilruth. Spacecraft: Mercury.
  A series of meetings were held in Washington, with Robert R. Gilruth serving as chairman to draft a manned satellite program and provide a basic plan for meeting the objectives of this program. Others attending included S. B. Batdorf, A. J. Eggers, Maxime A. Faget, George Low, Warren North, Walter C. Williams, and Robert C. Youngquist.

1959 April 9-28 - .

• Research Steering Committee on Manned Space Flight members nominated - . Nation: USA. Related Persons: Faget, Low, George. Program: Apollo.
  Members of the new Research Steering Committee on Manned Space Flight were nominated by the Ames, Lewis, and Langley Research Centers, the High Speed Flight Station (HSFS) (later Flight Research Center), the Jet Propulsion Laboratory (JPL), the Office of Space Flight Development OSFD), and the Office of Aeronautical and Space Research (OASR). They were: Alfred J. Eggers, Jr. (Ames); Bruce T. Lundin (Lewis); Laurence K. Loftin, Jr. (Langley); De E. Beeler (HSFS); Harris M. Schurmeier (JPL); Maxime A. Faget (STG) ; George M. Low of NASA Headquarters OSFD) ; and Milton B. Ames, Jr. (part-time) (OASR).

1959 May 25-26 - .

• First meeting of the Research Steering Committee on Manned Space Flight - . Nation: USA. Related Persons: Faget, Goett, Low, George. Program: Apollo. Spacecraft: Mercury.
  The first meeting of the Research Steering Committee on Manned Space Flight was held at NASA Headquarters. Members of the Committee attending were: Harry J. Goett, Chairman; Milton B. Ames, Jr. (part-time); De E. Beeler; Alfred J. Eggers, Jr.; Maxime A. Faget; Laurence K. Loftin, Jr.; George M. Low; Bruce T. Lundin; and Harris M. Schurmeier. Observers were John H. Disher, Robert M. Crane, Warren J. North, Milton W. Rosen (part-time), and H. Kurt Strass.
  The purpose of the Committee was to take a long-term look at man-in-space problems, leading eventually to recommendations on future missions and on broad aspects of Center research programs to ensure that the Centers were providing proper information. Committee investigations would range beyond Mercury and Dyna-Soar but would not be overly concerned with specific vehicular configurations. The Committee would report directly to the Office of Aeronautical and Space Research.

1959 May 25-26 - . LV Family: Saturn I. Launch Vehicle: Saturn C-2.

• National booster program, Dyna-Soar, and Mercury discussed - . Nation: USA. Related Persons: Faget, Low, George. Program: Apollo. Spacecraft: Mercury.
  The national booster program, Dyna-Soar, and Project Mercury were discussed by the Research Steering Committee. Members also presented reviews of Center programs related to manned space flight. Maxime A. Faget of STG endorsed lunar exploration as the present goal of the Committee although recognizing the end objective as manned interplanetary travel. George M. Low of NASA Headquarters recommended that the Committee:
  • Adopt the lunar landing mission as its long-range objective.
  • Investigate vehicle staging so that Saturn could be used for manned lunar landings without complete reliance on Nova.
  • Make a study of whether parachute or airport landing techniques should be emphasized.
  • Consider nuclear rocket propulsion possibilities for space flight.
  • Attach importance to research on auxiliary power plants such as hydrogen-oxygen systems.

1959 May 27 - .

• STG staff discusses the possibility of an advanced manned spacecraft - . Nation: USA. Related Persons: Chamberlin, Faget, Gilruth, Low, George. Program: Apollo.
  Director Robert R. Gilruth met with members of his STG staff (Paul E. Purser, Charles J. Donlan, James A. Chamberlin, Raymond L. Zavasky, W. Kemble Johnson, Charles W. Mathews, Maxime A. Faget, and Charles H. Zimmeman) and George M. Low from NASA Headquarters to discuss the possibility of an advanced manned spacecraft.

1959 July 6 - .

• Mercury spacecraft energetic particles research. - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  As a result of a discussion between Maxime A. Faget, Space Task Group, and John E. Naugle, Space Science Division, NASA Headquarters, it was concluded that there were several important scientific experiments in the field of energetic particles research that could be performed by placing packets of emulsion within the Mercury spacecraft. Work was started to determine a suitable packet location, along with other details associated with conducting such experiments.

1959 November 2 - .

• Planning of advanced spacecraft systems begun - . Nation: USA. Related Persons: Chamberlin, Faget, Gilruth, Johnson, Caldwell. Program: Apollo.
  At an STG meeting, it was decided to begin planning of advanced spacecraft systems. Three primary assignments were made:
  1. The preliminary design of a multi-man (probably three-man) capsule for a circumlunar mission, with particular attention to the use of the capsule as a temporary space laboratory, lunar landing cabin, and deep-space probe;
  2. Mission analysis studies to establish exit and reentry corridors, weights, and propulsion requirements;
  3. Test program planning to decide on the number and purpose of launches.
     Additional Details: here....

1960 January - .

• Name Apollo suggested - . Nation: USA. Related Persons: Faget, Gilruth, Silverstein. Program: Apollo. Spacecraft: Apollo CSM.
  At a luncheon in Washington, Abe Silverstein, Director of the Office of Space Flight Programs, suggested the name "Apollo" for the manned space flight program that was to follow Mercury. Others at the luncheon were Don R. Ostrander from NASA Headquarters and Robert R. Gilruth, Maxime A. Faget, and Charles J. Donlan from STG.

1960 April 1-May 3 - .

• Advanced manned spacecraft program guidelines for aborted missions and landing - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Recovery, CSM Source Selection.
  In discussing the advanced manned spacecraft program at NASA Centers, Maxime A. Faget of STG detailed the guidelines for aborted missions and landing:
  1. The spacecraft must have a capability of safe crew recovery from aborted missions at any speed up to the maximum velocity, this capability to be independent of the launch propulsion system.
  2. A satisfactory landing by the spacecraft on both water and land, avoiding local hazards in the recovery area, was necessary. This requirement was predicated on two considerations: emergency conditions or navigation errors could force a landing on either water or land; and accessibility for recovery and the relative superiority of land versus water landing would depend on local conditions and other factors. The spacecraft should be able to land in a 30-knot wind, be watertight, and be seaworthy under conditions of 10- to 12-foot waves.
  3. Planned landing capability by the spacecraft at one of several previously designated ground surface locations, each approximately 10 square miles in area, would be necessary. Studies were needed to assess the value of impulse maneuvers, guidance quality, and aerodynamic lift over drag during the return from the lunar mission. Faget pointed out that this requirement was far less severe for the earth orbit mission than for the lunar return.
  4. The spacecraft design should provide for crew survival for at least 72 hours after landing. Because of the unpredictability of possible emergency maneuvers, it would be impossible to provide sufficient recovery forces to cover all possible landing locations. The 72-hour requirement would permit mobilization of normally existing facilities and enough time for safe recovery. Locating devices on the spacecraft should perform adequately anywhere in the world.
  5. Auxiliary propulsion should be provided for guidance maneuvers needed to effect a safe return in a launch emergency. Accuracy and capability of the guidance system should be studied to determine auxiliary propulsion requirements. Sufficient reserve propulsion should be included to accommodate corrections for maximum guidance errors. The single system could serve for either guidance maneuvers or escape propulsion requirements.

1960 May 5 - .

• STG and Grumman discuss advanced spacecraft programs - . Nation: USA. Related Persons: Chamberlin, Faget, Gilruth. Program: Apollo. Spacecraft: Apollo LM, LM Source Selection.
  Robcrt R. Gilruth, Paul E. Purser, James A. Chamberlin, Maxime A. Faget, and H. Kurt Strass of STG met with a group from the Grumman Aircraft Engineering Corporation to discuss advanced spacecraft programs. Grumman had been working on guidance requirements for circumlunar flights under the sponsorship of the Navy and presented Strass with a report of this work.

1960 September 1 - .

• Apollo Project Office formed - . Nation: USA. Related Persons: Faget. Program: Apollo.
  In an organizational change within STG, Maxime A. Faget was appointed Chief of the Flight Systems Division and Robert O. Piland was named Assistant Chief for Advanced Projects. The Apollo Project Office was formed with Piland as Head of the Office; members included John B. Lee, J. Thomas Markley, William W. Petynia,and H. Kurt Strass.

1960 October 4 - .

• Evaluation Boards formed to consider industry proposals for Apollo spacecraft - . Nation: USA. Related Persons: Faget, Goett. Program: Apollo. Spacecraft: Apollo CSM, CSM Source Selection.
  Members were appointed to the Technical Assessment Panels and the Evaluation Board to consider industry proposals for Apollo spacecraft feasibility studies. Members of the Evaluation Board were: Charles J. Donlan (STG), Chairman; Maxime A. Faget (STG) ; Robert O. Piland (STG), Secretary; John H. Disher (NASA Headquarters Office of Space Flight Programs); Alvin Seiff (Ames); John V. Becker (Langley); H. H. Koelle (Marshall); Harry J. Goett (Goddard), ex officio; and Robert R. Gilruth (STG), ex officio.

1960 November 29 - .

• Briefing on the Apollo and Saturn programs - . Nation: USA. Related Persons: Faget, von Braun. Program: Apollo. Spacecraft: Apollo CSM, CSM Source Selection, LM Mode Debate, LM Source Selection.
  A joint briefing on the Apollo and Saturn programs was held at Marshall Space Flight Center MSFC, attended by representatives of STG and MSFC. Maxime A. Faget of STG and MSFC Director Wernher von Braun agreed that a joint STG-MSFC program would be developed to accomplish a manned lunar landing. Areas of responsibility were: MSFC launch vehicle and landing on the moon; STG - lunar orbit, landing, and return to earth.

1961 January 5-6 - .

• Manned lunar landing discussed with Space Exploration Program Council - . Nation: USA. Related Persons: Faget, von Braun. Program: Apollo. Spacecraft: Apollo LM, LM Mode Debate, LM Source Selection.
  During a meeting of the Space Exploration Program Council at NASA Headquarters, the subject of a manned lunar landing was discussed. Following presentations on earth orbit rendezvous (Wernher von Braun, Director of Marshall Space Flight Center), lunar orbit rendezvous (John C. Houbolt of Langley Research Center), and direct ascent (Melvyn Savage of NASA Headquarters), the Council decided that NASA should not follow any one of these specific approaches, but should proceed on a broad base to afford flexibility. Another outcome of the discussion was an agreement that NASA should have an orbital rendezvous program which could stand alone as well as being a part of the manned lunar program. A task group was named to define the elements of the program insofar as possible. Members of the group were George M. Low, Chairman, Eldon W. Hall, A. M. Mayo, Ernest O. Pearson, Jr., and Oran W. Nicks, all of NASA Headquarters; Maxime A. Faget of STG; and H. H. Koelle of Marshall Space Flight Center. This group became known as the Low Committee.

1961 February 13 - .

• NASA and McDonnell began discussions of an advanced Mercury spacecraft. - . Nation: USA. Related Persons: Chamberlin, Faget, Gilruth. Spacecraft: Gemini.
  McDonnell had been studying the concept of a maneuverable Mercury spacecraft since 1959. On February 1, Space Task Group (STG) Director Robert R. Gilruth assigned James A. Chamberlin, Chief, STG Engineering Division, who had been working with McDonnell on Mercury for more than a year, to institute studies with McDonnell on improving Mercury for future manned space flight programs. Additional Details: here....

1961 June 2 - .

• Project Apollo plans and programs meeting - . Nation: USA. Related Persons: Chamberlin, Faget. Program: Apollo.
  A meeting to discuss Project Apollo plans and programs was held at NASA Headquarters. Abe Silverstein, Warren J. North, John H. Disher, and George M. Low of NASA Headquarters and Robert R. Gilruth, Walter C. Williams, Maxime A. Faget, James A. Chamberlin, and Robert O. Piland of STG participated in the discussions. Six prime contract areas were defined: spacecraft (command center), onboard propulsion, lunar landing propulsion, launch vehicle (probably several prime contracts), tracking and communications network, and launch facilities and equipment. The prime contractor for the spacecraft would be responsible for the design, engineering, and fabrication of the spacecraft; for the integration of the onboard and lunar landing propulsion systems: and for the integration of the entire spacecraft system with the launch vehicle. In connection with the prime contract, STG would:
  • Define details for specifications and justify choices
  • Prepare a "scope of work" statement for release to industry by July 1
  • Prepare spacecraft specifications for release by August 1
  • Set up a contract evaluation team, qualified to evaluate the technical, management, design, engineering, and fabrication capabilities of the bidders.
    In connection with other projects directly relating to the Apollo program, STG was to:
  • Forward to Marshall Space Flight Center, via the Office of Space Flight Programs, the spacecraft systems part of a preliminary development plan for Saturn reentry tests
  • Make recommendations on an advanced version of the Mercury capsule
  • Designate a liaison member for the Lunar Sciences Subcommittee of the Space Sciences Steering Committee.
    The Office of Space Flight Programs would arrange a meeting with the Office of Advanced Research Programs, STG, and Langley Research Center on the Atlas-Agena reentry tests and with the Office of Advanced Research Programs, Office of Life Sciences Programs, STG, and Ames Research Center on the biomedical flight program.

1961 June 5 - .

• The Flight Vehicles Integration Branch was organized within STG - . Nation: USA. Related Persons: Faget. Program: Apollo.
  The Flight Vehicles Integration Branch was organized within STG. Members included H. Kurt Strass, Robert L. O'Neal, and Charles H. Wilson. Maxime A. Faget, Chief, Flight Systems Division, also served as temporary Branch Chief. The Branch was to provide technical aid to STG in solving compatibility requirements for spacecraft and launch vehicles for manned flight missions.

1961 June 26 - .

• Langley Research Center lunar landing paper - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM, LM Mode Debate, LM Source Selection.
  Maxime A. Faget, Paul E. Purser, and Charles J. Donlan of STG met with Arthur W. Vogeley, Clinton E. Brown, and Laurence K. Loftin, Jr., of Langley Research Center on a "lunar landing" paper. Faget's outline was to be used, with part of the information to be worked up by Vogeley.

1961 July 28 - .

• Source Evaluation Board to evaluate contractors' proposals for the Apollo spacecraft - . Nation: USA. Related Persons: Chamberlin, Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Source Selection.
  NASA Associate Administrator Robert C. Seamans, Jr., appointed members to the Source Evaluation Board to evaluate contractors' proposals for the Apollo spacecraft. Walter C. Williams of STG served as Chairman, and members included Robert O. Piland, Wesley L. Hjornevik, Maxime A. Faget, James A. Chamberlin, Charles W. Mathews, and Dave W. Lang, all of STG; George M. Low, Brooks C. Preacher, and James T. Koppenhaver (nonvoting member) from NASA Headquarters; and Oswald H. Lange from Marshall Space Flight Center. On November 2, Faget became the Chairman, Kenneth S. Kleinknecht was added as a member, and Williams was relieved from his assignment.

1962 March 15-16 - .

• First monthly meeting of the Apollo design and review team to survey NAA's progress - . Nation: USA. Related Persons: Faget, Kraft, Maynard. Program: Apollo. Spacecraft: Apollo CSM, CSM Fuel Cell, CSM Heat Shield.
  Charles W. Frick, Manager of the MSC Apollo Spacecraft Project Office, together with Maxime A. Faget, Charles W. Mathews, Christopher C. Kraft, Jr., John B. Lee, Owen E. Maynard, and Alan B. Kehlet of MSC and George M. Low of the NASA Office of Manned Space Flight, visited NAA at Downey, Calif. This was the first monthly meeting of the Apollo design and review team to survey NAA's progress in various areas, including the Apollo spacecraft heatshield, fuel cells, and service module.

1962 October 25 - .

• NASA Outstanding Leadership Awards - . Nation: USA. Related Persons: Faget. Spacecraft: Mercury.
  NASA Associate Administrator Robert C. Seamans, Jr., presented Outstanding Leadership Awards to Maxime A. Faget, Assistant Director for Engineering and Development, Manned Spacecraft Center, and George B. Graves, Jr., Assistant Director for Information and Control Systems. Also, at the NASA annual awards ceremony the Administrator, James E. Webb, presented Group Achievement Awards to four Manned Spacecraft Center activities: Assistant Directorate for Engineering and Development, Preflight Operations Division, Mercury Project Office, and Flight Operations Division.

1962 December 4 - .

• NASA Mercury monetary awards to seven individuals - . Nation: USA. Related Persons: Faget, Johnson, Caldwell. Spacecraft: Mercury.
  Information was received from the NASA Inventions and Contributions activity that seven individuals, a majority of whom were still associated with the Manned Spacecraft Center, would receive monetary awards for inventions that were important in the development of Project Mercury. These were: Andre Meyer ($1,000) for the vehicle parachute and equipment jettison equipment; Maxime Faget and Andre Meyer (divided 1,500)fortheemergencyejectiondevice;MaximeFaget,WilliamBland,andJackHeberlig(divided1,500) for the emergency ejection device; Maxime Faget, William Bland, and Jack Heberlig (divided 1,500)fortheemergencyejectiondevice;MaximeFaget,WilliamBland,andJackHeberlig(divided2,000) for the survival couch; and Maxime Faget, Andre Meyer, Robert Chilton, Williard Blanchard, Alan Kehlet, Jerome Hammack, and Caldwell Johnson (divided $4,200) for the spacecraft design. Formal presentation of these awards was made on December 10, 1962.

1963 September 4 - .

• Manned Spacecraft Criteria Board - . Nation: USA. Related Persons: Chamberlin, Faget. Program: Apollo.
  Director Robert R. Gilruth established the MSC Manned Spacecraft Criteria Board to set up engineering, design, and procedural standards for manned spacecraft and associated systems. The board was composed of Maxime A. Faget, Chairman; James A. Chamberlin; Kenneth S. Kleinknecht; F. John Bailey, Jr.; G. Barry Graves; Jacob C. Moser; and Norman F. Smith, Secretary. Board criteria would become MSC policy; and - unless specific waivers were obtained, compliance by project offices was mandatory.

1963 November 5 - .

• Reorganization of MSC - . Nation: USA. Related Persons: Faget, Kraft, Shea, Slayton. Program: Apollo. Spacecraft: Gemini.
  MSC Director Robert R. Gilruth announced a reorganization of MSC to strengthen the management of the Apollo and Gemini programs. Under Gilruth and Deputy Director James C. Elms, there were now four Assistant Directors, Managers for both the Gemini and Apollo programs, and a Manager for MSC's Florida Operations. Assigned to these positions were:
  Maxime A. Faget, Assistant Director for Engineering and Development Christopher C. Kraft, Jr., Assistant Director for Flight Operations Donald K. Slayton, Assistant Director for Flight Crew Operations Wesley L. Hjornevik, Assistant Director for Administration Joseph F. Shea, Manager, Apollo Spacecraft Program Office Charles W. Mathews, Manager, Gemini Program Office and G. Merritt Preston, Manager, MSC Florida Operations.

1964 January 15 - .

• Phase II follow-on extended Apollo system studies. - . Nation: USA. Related Persons: Faget. Spacecraft Bus: Apollo CSM. Spacecraft: Apollo X.
  Following completion of feasibility studies of an extended Apollo system at MSC, Edward Z. Gray, Advanced Manned Missions Program Director at Headquarters, told MSC's Maxime A. Faget, Director of Engineering and Development, to go ahead with phase II follow-on studies. Gray presented guidelines and suggested tasks for such a study, citing his desire for two separate contracts to industry to study the command and service modules and various concepts for laboratory modules.

1964 February 1 - .

• Apollo Program Review told that metabolic rate in an unpressurized suit twice that in clothes - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM, LM ECS, LM Weight.
  At an Apollo Program Review held at MSC, Maxime A. Faget reported that Crew Systems Division had learned that the metabolic rate of a man walking in an unpressurized suit was twice that of a man in everyday clothes. When the suit was pressurized to 1.8 newtons per square centimeter (3.5 psi), the rate was about four times as much. To counteract this, a watercooled undergarment developed by the British Ministry of Aviation's Royal Aircraft Establishment was being tested at Hamilton Standard. These "space-age long johns" had a network of small tubes through which water circulated and absorbed body heat. Advantages of the system were improved heat transfer, low circulating noise levels, and relatively moderate flow rates required. An MSC study on integration of the suit with the LEM environmental control system showed a possible weight savings of 9 kilograms (20 pounds).

1964 October 5-8 - .

• Formal review of the Apollo LEM mockup M-5 - . Nation: USA. Related Persons: Faget, Kraft, Slayton. Program: Apollo. Spacecraft: Apollo LM, LM Ascent Propulsion, LM Descent Propulsion, LM Electrical, LM Landing Gear.
  NASA conducted a formal review of the LEM mockup M-5 at the Grumman factory. This inspection was intended to affirm that the M-5 configuration reflected all design requirements and to definitize the LEM configuration. Members of the Mockup Review Board were Chairman Owen E. Maynard, Chief, Systems Engineering Division, ASPO; R. W. Carbee, LEM Subsystem Project Engineer, Grumman; Maxime A. Faget, Assistant Director for Engineering and Development, MSC; Thomas J. Kelly, LEM Project Engineer, Grumman; Christopher C. Kraft, Jr. (represented by Sigurd A. Sjoberg), Assistant Director for Flight Operations, MSC; Owen G. Morris, Chief, Reliability and Quality Assurance Division, ASPO; William F. Rector III, LEM Project Officer, ASPO; and Donald K. Slayton, Assistant Director for Flight Crew Operations, MSC.
  The astronauts' review was held on October 5 and 6. It included demonstrations of entering and getting out of the LEM, techniques for climbing and descending the ladder, and crew mobility inside the spacecraft. The general inspection was held on the 7th and the Review Board met on the 8th. Those attending the review used request for change (RFC) forms to propose spacecraft design alterations. Before submission to the Board, these requests were discussed by contractor personnel and NASA coordinators to assess their effect upon system design, interfaces, weight, and reliability.
  The inspection categories were crew provisions; controls, displays, and lighting; the stabilization and control system and the guidance and navigation radar; electrical power; propulsion (ascent, descent, reaction control system, and pyrotechnics ; power generation cryogenic storage and fuel cell assemblies ; environmental control; communications and instrumentation; structures and landing gear; scientific equipment; and reliability and quality' control. A total of 148 RFCs were submitted. Most were aimed at enhancing the spacecraft's operational capability; considerable attention also was given to quality and reliability and to ground checkout of various systems. No major redesigns of the configuration were suggested.
  As a result of this review, the Board recommended that Grumman take immediate action on those RFC's which it had approved. Further, the LEM contractor and MSC should promptly investigate those items which the Board had assigned for further study. On the basis of the revised M-5 configuration, Grumman could proceed with LEM development and qualification. This updated mockup would be the basis for tooling and fabrication of the initial hardware as well.

1964 November 25 - .

• Apollo LEM descent engine subcontractors reviewed - . Nation: USA. Related Persons: Faget, Shea. Program: Apollo. Spacecraft: Apollo LM, LM Descent Propulsion.
  ASPO Manager Joseph F. Shea informed Apollo Program Director Samuel C. Phillips that it was his desire to review the progress of the two subcontractors (Space Technology Laboratory and Rocketdyne) prior to the final evaluation and selection of a subcontractor for the LEM descent engine.
  Shea had asked MSC's Maxime A. Faget to be chairman of a committee to accomplish the review, and would also ask the following individuals to serve: C. H. Lambert, W. F. Rector III, and J. G. Thibodaux, all of MSC; L. F. Belew, MSFC; M. Dandridge and J. A. Gavin, Grumman; I. A. Johnsen, Lewis Research Center; C. H. King, OMSF; Maj. W. R. Moe, Edwards Rocket Research Laboratory; and A. O. Tischler, NASA Office of Advanced Research and Technology.
  The Committee should
  1. establish review criteria during a planning meeting at MSC during the week of November 30, 1964;
  2. visit the two subcontractors' facilities during the week of December 7, 1964, for review of technical status, manufacturing resources, and test facilities; and
  3. prepare a written report and brief appropriate NASA personnel on their findings by December 18, 1964.
     "Both GAEC and NASA will be parties to the final selection and it is not my intent to usurp GAEC's responsibility in this matter; but I do feel we should have the intelligence at our disposal to appreciate all ramifications of GAEC's final selection," Shea said.

1965 May 4 - .

• Plans for Fiscal Year 1966 Apollo Extension System program definition and development. - . Nation: USA. Related Persons: Faget. Spacecraft Bus: Apollo CSM. Spacecraft: Apollo X.
  MSC Assistant Director for Engineering and Development Maxime A. Faget submitted to NASA Hq the Center's plans for Fiscal Year 1966 Apollo Extension System program definition and subsystems development efforts. The information submitted was based on MSC's AES study and supporting development efforts and was broken down into several categories in line with guidelines laid down by the Office of Manned Space Flight: program definition, verification of the capabilities of Apollo subsystems for AES; definition and initial development of experiment payloads and payload support; long leadtime development of primary spacecraft systems critical to achieving minimum AES objectives (i.e., four to six weeks orbital capability and up to two weeks on the lunar surface); and development of improved or alternate subsystems that would extend AES capabilities up to three months in Earth orbit. Tasks in support of these objectives, Faget stated, fell into two priorities: (1) those tasks required to verify an early AES capability; and (2) tasks in support of later AES missions and for system improvement. Those tasks having immediate priority, therefore, demanded the 'hard core' of AES funding essential to meet the early AES flight dates.

1965 July 14 - .

• Advisory group on the Apollo Lunar Sample Receiving Laboratory - . Nation: USA. Related Persons: Faget. Program: Apollo.
  Willis B. Foster, NASA's Director of Manned Space Science Programs, informed MSC's Maxime A. Faget that he had asked the following persons to continue to serve as members of an Ad Hoc Committee as an advisory group to Foster with regard to the design and construction of the Lunar Sample Receiving Laboratory: E. C. T. Chao (Chairman), Lorin Clark (alternate chairman), James Arnold, Clifford Frondel, Briggs Phillips, P. R. Bell, and alternates Jonathan Klein and Larry Hall.

1966 February 1 - .

• Lunar Orbiter program status - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Lunar Orbiter.
  MCC's Robert R. Gilruth, Maxime A. Faget, and William E. Stoney visited Langley Research Center to discuss the Orbiter program status and plans for distributing photos obtained from Orbiter with Floyd Thompson, Charles Donlan, and other Langley personnel members connected with the Orbiter program. Important aspects of the program were presented, with particular emphasis on the camera system and the kind and quality of photography to be obtained. In the discussion of data handling it was apparent there were no conflicts of purpose or planned activity between LaRC and MSC. It was determined that strong MSC representation at Langley during the photo screening period would be advantageous to MSC and of great benefit in MSC's subsequent lunar landing site evaluation.

1966 April 21 - .

• MSC announced the establishment of an Apollo Flight Experiment Board - . Nation: USA. Related Persons: Faget, Kraft, Slayton. Program: Apollo.
  MSC announced the establishment of a Flight Experiment Board. The Board would select and recommend to the Director space flight experiments proposed from within the Center and judged by the Board to be in the best interest of the Center and the NASA space flight program. MSC-originated flight experiments were expected normally to be designated as one of two general classifications: Type I - Medical, Space Science, Flight Operations or Engineering that would yield new knowledge or improve the state of the art; Type II - Operational, which would be required in direct support of major manned flight programs such as Apollo.
  Members appointed to the Board were George M. Low, chairman; Warren Gillespie, Jr., executive secretary; Maxime A. Faget; Robert O. Piland; Charles A. Berry; Christopher C. Kraft, Jr.; Donald K. Slayton; Kenneth S. Kleinknecht; and Joseph N. Kotanchik. The Board would meet bimonthly on the first Friday of every even month, with called meetings at the direction of the chairman when necessary to expedite experiments.

1966 May 11 - .

• Plans for Apollo space rescue discontinued - . Nation: USA. Related Persons: Faget, Low, George. Program: Apollo. Spacecraft: Apollo Lunar Landing, Gemini Lunar Surface Rescue Spacecraft.
  MSC Deputy Director George M. Low recommended to Maxime A. Faget, MSC, that, in light of Air Force and Aerospace Corp. studies on space rescue, MSC plans for a general study on space rescue be discontinued and a formal request be made to OMSF to cancel the request for proposals, which had not yet been released. As an alternative, Low suggested that MSC should cooperate with the Air Force to maximize gains from the USAF task on space rescue requirements.

1966 July 9 - .

• Reservations on a synchronous-orbit mission for AAP. - . Nation: USA. Related Persons: Faget, Low, George. Spacecraft Bus: Apollo CSM. Spacecraft: Apollo X.
  George M. Low expressed his reservations about the validity of planning a synchronous-orbit mission for AAP. In a note to Maxime A. Faget, Low commented on the recent interest in such a mission and voiced his own doubt concerning either the need for or the desirability of such a flight. Low stated that such things as synoptic views of terrain or weather phenomena could be done just as well from low Earth orbit using mosaic techniques. Moreover, low orbits afforded simpler operations, much greater payload capabilities, and minimal radiation hazards. Low asked Faget to have his organization prepare an analysis of low Earth-orbit versus synchronous- orbit operations in preparation for upcoming AAP planning discussions in Washington at the end of the month.

1966 August 5 - .

• Stowable net couches for Apollo - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Cockpit.
  Maxime A. Faget, MSC, informed Center Director Robert R. Gilruth there was a continuing effort on lightweight, energy-absorbing, and stowable net couches, and development had been redirected to a nonelastic fabric net couch system attached to existing Apollo attenuation struts. North American Aviation had previously been given the task of investigating the use of net couches on Apollo. Results of that investigation indicated the spacecraft attenuation-strut-vehicle attachments would be overloaded when using net couches. The North American Aviation investigators made their calculations by assuming no-man attenuation in the lateral and longitudinal force directions. Those calculations were recomputed using the design criteria and proper loadings and the results indicated no overloading when using net couches. MSC's Advanced Spacecraft Technology Division had reviewed and approved the efforts, permitting use of the net couches on Apollo and Apollo Applications missions.

1967 January 23 - .

• Apollo Lunar Mission Planning Board - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM, LM Television.
  The Lunar Mission Planning Board held its first meeting at MSC. Present, in addition to Chairman Robert R. Gilruth, were Charles A. Berry, Maxime A. Faget, George M. Low, Robert O. Piland, Wesley L. Hjornevik, and acting secretary William E. Stoney, Jr., all of MSC. Principal subject of discussion was the photography obtained by Lunar Orbiter I and Lunar Orbiter II and application of this photography to Apollo site selection. The material was presented by John Eggleston and Owen Maynard, both of MSC. Orbiter I had obtained medium-resolution photography of sites on the southern half of the Apollo area of interest; Orbiter II had obtained both medium- and high-resolution photographs of sites toward the northern half of the area. Several action items were assigned, with progress to be reported at the next meeting, including a definition of requirements for a TV landing aid for the lunar module and a report on landing-site-selection restraints based on data available from Lunar Orbiter I and II only, and another on data from Lunar Orbiter I, II, and III.

1967 January 30 - .

• Additional Apollo 204 Review Board consultants - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Robert W. Van Dolah of the Bureau of Mines, I. Irving Pinkel of Lewis Research Center, and Thomas G. Horeff of the Federal Aviation Agency joined the Apollo 204 Review Board as consultants. . Additional Details: here....

1967 February 4 - .

• Draft report on the use of internal and external power for the Apollo 204 Review Board - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Spacecraft: Apollo CSM, CSM Block I. Maxime Faget, MSC, distributed a draft report on the use of internal and external power on the command module for the information of the Apollo 204 Review Board. . Additional Details: here....

1967 February 7 - .

• Apollo 204 Review Board established 21 Task Panels - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Floyd L. Thompson, Chairman of the Apollo 204 Review Board, formally established 21 task panels to support the investigation. . Additional Details: here....

1967 March 1 - .

• Apollo 204 Review Board designates custodian for the Review Board material - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Apollo 204 Review Board Chairman Floyd Thompson announced that the NASA Deputy Administrator had signed a memorandum February 27 designating the Director, Langley Research Center, custodian of the Review Board material. . Additional Details: here....

1967 March 8 - .

• Apollo 204 Review Board follow-up report - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204.
  Maxime A. Faget, MSC, presented the Apollo 204 Review Board a follow-up report on analysis of the arc indication on the lower-equipment-bay junction-box cover plate. The plate had been delivered to the KSC Material Analysis Laboratory and, in addition to the analysis of the arc indication, molten material found on the bottom of the plate would also be analyzed.

1967 March 28 - .

• Apollo 204 Review Board asked for a report on the Pyrotechnic Installation Building activity - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Spacecraft: Apollo CSM, CSM Block I. Apollo 204 Review Board Chairman Floyd Thompson asked for a report on the Pyrotechnic Installation Building activity. . Additional Details: here....

1967 April 18 - .

• No NASA accountability for Apollo wiring - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Electrical.
  ASPO Manager George M. Low pointed out to MSC Director of Engineering and Development Maxime A. Faget that apparently no single person at MSC was responsible for spacecraft wiring. Low said he would like to discuss naming a subsystem manager to follow this general area, including not only the wiring schematics, circuitry, circuit-breaker protection, etc., but also the detailed design, engineering, fabrication, and installation of wiring harnesses.

1967 May 5 - .

• Circuit breakers in Apollo were flammable - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM, CSM Electrical, LM Electrical.
  Circuit breakers being used in both CSM and LM were flammable, MSC ASPO Manager George Low told Engineering and Development Director Maxime A. Faget. Low said that although Structures and Mechanics Division was developing a coating to be applied to the circuit breakers, such a solution was not the best for the long run. He requested that the Instrumentation and Electronics Systems Division find replacement circuit breakers for Apollo - ideally, circuit breakers that would not bum and that would fit within the same volume as the existing ones, permitting replacement in panels already built. On July 12 Low wrote Faget again: "In light of the work that has gone on since my May 5, 1967, memo, are you now prepared to propose the use of metal-jacketed circuit breakers for Apollo spacecraft? If the answer is affirmative, then we should get specific direction to our contractors immediately. Also, have you surveyed the industry to see whether a replacement circuit breaker is available or will be available in the future?" Low requested an early reply.

1967 May 12 - .

• Apollo 204 Review Board subcommittee to examine the final report of Panel 18 - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 204. Apollo 204 Review Board Chairman Floyd L. Thompson appointed a subcommittee to examine the final report of Panel 18 and prepare recommendations regarding its acceptability for inclusion in the Board's Report. . Additional Details: here....

1967 June 17 - .

• Plans made to armor-plate 102 out of 167 solder joints inside the Apollo CM of spacecraft 101 - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 7. Spacecraft: Apollo CSM, CSM Block II. Plans were to armor-plate 102 out of 167 solder joints inside the CM of spacecraft 101, ASPO Manager George M. Low informed Maxime A. Faget, MSC's Director of Engineering and Development. . Additional Details: here....

1967 September 26 - .

• Flammability Test Review Board for Apollo LM M-6 - . Nation: USA. Related Persons: Faget, Kraft. Program: Apollo. Spacecraft: Apollo LM, LM Crew Station.
  The Flammability Test Review Board met at MSC to determine if the M-6 vehicle (a full-scale mockup of the LM cabin interior) was ready for test and that the ignition points, configuration, instrumentation, and test facility were acceptable for verifying the fire safety of LTA-8 and LM-2 vehicles. Additional Details: here....

1967 September 29 - .

• Board to review the Apollo operational corridor - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Heat Shield.
  An Apollo Entry Performance Review Board was established by the MSC Director to review and validate the analytical tools as well as the Apollo operational corridor. The Board was set up because the performance of the ablation heatshield in the Apollo spacecraft, as then analyzed, imposed a limitation on the entry corridor at lunar return velocity. The following were named to the Board: Maxime A. Faget, MSC, chairman; Kenneth S. Kleinknecht, MSC; Eugene C. Draley and Don D. Davis, Jr., Langley Research Center; Alvin Seiff and Glen Goodwin, Ames Research Center; and Leo T. Chauvin, MSC, secretary.

1967 October 13 - .

• Apollo Spacecraft Configuration Control Board reins in changes - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 9. Spacecraft: Apollo LM. In an effort to keep a tight rein on changes made in spacecraft, the Apollo Spacecraft Configuration Control Board (CCB) established ground rules.. Additional Details: here....

1967 October 18 - .

• Apollo Configuration Control Panel for GFE - . Nation: USA. Related Persons: Chamberlin, Faget. Program: Apollo.
  MSC's Director of Engineering and Development Maxime A. Faget, at the request of the ASPO Manager, established a Configuration Control Panel (CCP) for government furnished equipment (GFE). The panel would integrate control of changes in the GFE items supplied for the Apollo spacecraft. "Authority to bring change recommendations to the GFE Panel will be invested in Division Chiefs. Changes rejected by the Division Chiefs need not be reviewed by the GFE CCP," the memorandum establishing the panel said. Membership on the panel was as follows: Chairman, Maxime A. Faget; Alternate Chairman, James A. Chamberlin; Members, Richard S. Johnston, Robert A. Gardiner, R. W. Sawyer (sic), and William C. Bradford. Secretary would be John B. See.

1967 November 2 - .

• Apollo LM insulation susceptible to degradation from cabin leakage during pressurized conditions - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 11. Spacecraft: Apollo LM, LM Structural. Maxime A. Faget, MSC Director of Engineering and Development, told the ASPO Manager that he had reviewed the LM insulation status and concluded that "the present design is susceptible to degradation from cabin leakage during pressurized conditions. . Additional Details: here....

1967 November 16 - .

• Status of Apollo environmental control unit - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM ECS. Robert R. Gilruth, George M. Low, and Maxime A. Faget, with other MSC personnel and North American Rockwell management officials visited AiResearch to review the status of the Apollo environmental control unit electronic components.. Additional Details: here....

1967 December 20 - .

• Coax cable problems in Apollo CSM 103 - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 10. Spacecraft: Apollo CSM, CSM Block II. As a part of the managers' technical status review, Dale Myers of North American Rockwell presented his analysis of fixes for the coax cable in spacecraft 103 and subsequent spacecraft. . Additional Details: here....

1968 January 13 - .

• Apollo Senior Flammability Review Board - . Nation: USA. Related Persons: Faget. Program: Apollo.
  The Senior Flammability Review Board met at MSC with Chairman Robert R. Gilruth, George M. Low, Maxime A. Faget, Aleck C. Bond, Charles A. Berry, Donald K. Slayton, Christopher C. Kraft, Jr., Kenneth S. Kleinknecht, all of MSC, and George Jeffs of North American Rockwell participating. The meeting summary reported that a 60-percent-oxygen and 40-percent-nitrogen atmosphere was acceptable from a crew physiological standpoint. The requirement for crew prebreathing before launch was not dependent upon launching with the atmosphere. Operationally, the crew could remove their helmets and gloves following orbital insertion and verification of the integrity of the cabin and its environmental control system; oxygen leakage would be allowed to enrich the crew compartment atmosphere.
  On January 25, Berry, MSC Director of Medical Research and Operations, mote Gilruth: "We do not concur in the stated finding of the Board that a 60 per cent oxygen, 40 per cent nitrogen atmosphere is acceptable from a crew physiological standpoint. While it is true that a 60% oxygen, 40% nitrogen atmosphere at 5.6 psi (3.9 newtons per sq cm) should result in a cabin atmosphere physiologically equivalent to sea level conditions, this will not be the case in a spacecraft launched with a 60% oxygen, 40% nitrogen atmosphere to which no oxygen is added except by normal operation of the cabin regulator. Oxygen will be metabolized by the crew at a much greater rate than nitrogen will be leaking from the spacecraft. Assuming a case in which cabin relief valve seats at 6 psi (4.1 newtons per sq cm) and the cabin regulator does not begin adding oxygen until 4.8 psi (3.3 newtons per sq cm), the cabin atmosphere would then consist of approximately 49% oxygen. This is physiologically equivalent to a 12,000-foot (3,700-meter) altitude in air. It would then take approximately 50 hours at the nominal cabin leak rate for the cabin regulator to enrich the mixture to a sea level equivalent."

1968 February 5 - .

• 40 per-cent nitrogen prelaunch atmosphere in Apollo - . Nation: USA. Related Persons: Faget, Slayton. Program: Apollo. Spacecraft: Apollo CSM, CSM Communications.
  A Senior Flammability Review Board meeting at MSC reached a number of decisions on the CSM. Attending were Robert R. Gilruth, chairman; George M. Low, Kenneth S. Kleinknecht, Aleck C. Bond, Maxime A. Faget, Donald K. Slayton, Charles A. Berry, and Rodney G. Rose, all of MSC; Samuel C. Phillips, NASA Hq.; William B. Bergen and Dale D. Myers, North American Rockwell; and George Stoner, Boeing (nonvoting observer).
  Several previous action assignments were reviewed:
  1. Component level Flammability Test Program - North American reviewed the results of its material identification and test program, the component test program, and the boilerplate 1,250 tests. These tests had provided the basis for design decisions on selection and application of CM nonmetallic materials.
  2. Boilerplate 1224 configuration comparison to CSMs 2TV-1 and 101 - North American presented the comparison and the Board decided that the boilerplate configuration was representative of the "worst case" configuration, considering both 2TV-l and 101.
  3. Internal ignition rationale - ignition rationale for the boilerplate 1224 tests was presented to the Board. Nichrome wire ignitors were used with the ignitor wire embedded in potting. In some locations a Ladicote cover was applied over the potting and ignitor. The Board pointed out that the ignition techniques were not really representative of actual operating conditions and were indeed overly severe.
  4. Crew communications umbilical - North American was evaluating a fluorel crew communications umbilical as well as fluorel oxygen umbilicals. A Beta sleeve over the oxygen and crew communications umbilicals would also be evaluated for its operational acceptability by the Crew.
     The Board presented a review of test results. In the tests at pressure of 4.3 newtons per square centimeter (6.2 pounds per square inch) in a 95-percent oxygen atmosphere, there were 38 ignitions in boilerplate 1224. Of these,5 produced fires large enough to require further consideration. In tests at 11.2 newtons per sq cm (16.2 psia) in a 60-percent-oxygen and 40-percent nitrogen atmosphere, there were 31 ignitions. Of these, 4 produced fires large enough to require further consideration.
     The Board concluded that the material changes made in the CM had resulted in a safe configuration in both the tested atmospheres. The Board agreed "that there will always be a degree of risk associated with manned space flight," but the risk of fire "was now substantially less than the basic risks inherent in manned space flight."
     Among decisions reached were:
  5. the CSM 2TV-1 and 101 coaxial cable configuration would be tested in the 60-percent-oxygen and 40-percent nitrogen atmosphere;
  6. material improvements and testing would be continued and changes would be phased in, pending the availability of proved materials; and
  7. action would be taken to be prepared to use a 60-percent-oxygen and 40-percent-nitrogen prelaunch atmosphere in CSM 101.
     A final decision would be made at the Design Certification Review on March 7.

1968 April 17 - .

• Numerous radiation detectors evaluated for Apollo - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Cockpit.
  MSC Engineering and Development Director Maxime Faget reported to George Low that his directorate had investigated numerous radiation detectors, ionization particle detectors, and chemical reactive detectors. The directorate had also obtained information from outside sources such as the National Bureau of Standards, Mine Safety Appliances, Parmalee Plastics, Wright-Patterson Air Force Base, and the Air Force Manned Orbiting Laboratory organization. None of the methods investigated could meet the stated requirements for a spacecraft fire detection system.

1968 May 13 - .

• Fire-in-the-hole test of the Apollo LM ascent engine issue deferred - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM, LM Ascent Propulsion.
  During an Apollo flight test program review at MSC, the question was left unresolved whether or not to perform a "fire-in-the-hole" test of the LM ascent engine (i.e., start the engine at the same instant the two stages of the spacecraft were disjoined - as the engine would have to be fired upon takeoff from the lunar surface) on either the D or E mission. Additional Details: here....

1968 June 7 - .

• Apollo LM descent stage heatshield and thermal blanket problems - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 11. Spacecraft: Apollo LM, LM Descent Propulsion.
  ASPO Manager George M. Low and others from MSC met with Grumman's LM engineering staff, headed by Thomas J. Kelly, to discuss the descent stage heatshield and thermal blanket problems associated with reduced thrust decay of the descent engine at lunar touchdown. Additional Details: here....

1968 June 10 - .

• Flight combustion stability monitor on Apollo 7 - . Nation: USA. Related Persons: Faget. Program: Apollo. Flight: Apollo 7. Spacecraft: Apollo CSM, CSM Block II.
  ASPO Manager George M. Low met with Christopher C. Kraft, Jr., and Donald K. Slayton, Directors of MSC Flight and Flight Crew Operations, and several members of their staffs (including astronaut Walter M. Schirra, Jr.) to discuss using the flight combustion stability monitor (FCSM) on the Apollo 7 flight. Additional Details: here....

1969 February 12 - .

• Apollo Operations Handbook review - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM.
  George M. Low, MSC, told Maxime A. Faget, MSC, that he had recently learned the Apollo Operations Handbook (AOH) was prepared for the Flight Crew Operations Directorate by prime contractors without any formalized review by engineering elements of MSC. On several occasions, when the Engineering and Development (E&D) subsystems managers looked at a section of the handbook in connection with problem areas they found the handbook in error. Low proposed that E&D should
  1. verify technical accuracy of the baseline issue of the handbook before its final issue for the F mission,
  2. verify all changes in the AOH in a timely manner, and
  3. verify any crew checklist changes made during the last 45 days before launch.

1969 February 27 - .

• Apollo Preliminary Lunar Landing Phase Photographic Operations Plan seriously deficient - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo LM.
  Maxime A. Faget, MSC Director of Engineering and Development, said he believed the Preliminary Lunar Landing Phase Photographic Operations Plan was seriously deficient in meeting its stated objectives. "From the standpoint of public information and historical documentation, I'm terribly disappointed to find that although 560 feet (170 meters) of movie film has been set aside for lunar surface use none will be exposed with the intent of providing first-class visual appreciation of the astronaut's activity on the moon during this singularly historical event. Everyone's impression of this occasion will be marred and distorted by the fact that the greatest frame rate is 12 frames per second. One can argue that 'suitable' (although jerky) motion rendition is produced by 'double-framing.' Nevertheless, it is almost unbelievable that the culmination of a 20 billion dollar program is to be recorded in such a stingy manner and the low-quality public information and historical material is in keeping with an otherwise high-quality program." Faget also noted he felt that, from a historical standpoint, both the lunar module pilot and the commander should be photographed with the Hasselblad camera while on the surface.

1969 March 6 - .

• Concern about Apollo software - . Nation: USA. Related Persons: Faget. Program: Apollo.
  NASA Associate Administrator for Manned Space Flight George E. Mueller, wrote MSC Director Robert R. Gilruth of his concern about Apollo software. "Software as I mean it to be understood in this letter includes computer programs, mission profiles and procedures (training). As I recall, the Apollo project started with a legacy of warnings from other programs about the rigors and pitfalls of software development. . . . I believe we are giving far more management attention to hardware changes than to software changes of similar impact." He questioned "whether some of these changes make the system better or safer when the disruptive effects of change are also considered. . . . We are making too many discretionary software changes. These are costing money and effort which could better be used elsewhere. . . ."
  Gilruth replied March 11: "I cannot agree with your contention that we are now controlling software with the same rigor and management attention that we are devoting to hardware changes. Our Apollo Spacecraft Program Office has organized a number of Configuration Control Boards at MSC. These include George Low's Apollo Spacecraft Configuration Control Board, Max Faget's Board for Government Furnished Equipment, Chris Kraft's Software Configuration Control Board, and Deke Slayton's Procedures Change Control Board. . . . Hardware changes . . . are directly under George Low's control. All computer program changes, both on board and on the ground, are controlled by Chris Kraft's Board. Changes to the Apollo Operations Handbook, flight crew procedures, crew checklists, trainers and simulators are controlled by Slayton. Changes in software or crew procedures that involve changes in schedule must additionally be approved by George Low's Board. The system I described is working well and, according to Sam Phillips, has resulted in a more disciplined change control than anywhere else in the Apollo Program. . . . We are not making discretionary software changes. We are only making those changes which our managers deem to be necessary in their effort to carry out the Apollo Program in the most effective manner."

1969 March 12 - .

• Status of a fire detection system for Apollo - . Nation: USA. Related Persons: Faget. Program: Apollo. Spacecraft: Apollo CSM, CSM Electrical.
  George M. Low discussed the status of a fire detection system for Apollo in a memorandum to Martin L. Raines, reminding him that such a system had been under consideration since the accident in January 1967. Low said: "Yesterday, Dr. (Maxime A.) Faget, you, and I participated in a meeting to review the current status of a flight fire detection system. It became quite clear that our state of knowledge about the physics and chemistry of fire in zero gravity is insufficient to permit the design and development of a flightworthy fire detection system at this time. For this reason, we agreed that we would not be able to incorporate a fire detection system in any of the Apollo spacecraft. We also agreed that it would be most worthwhile to continue the development of a detection system for future spacecraft."

2004 October 9 - .

• Death of Maxime A Faget - . Nation: Belize, USA. Related Persons: Faget. American Chief Designer of American manned spacecraft. Designed Mercury, Apollo, and Shuttle spacecraft..

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