STS-3 (original) (raw)


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z


STS-3


Part of STS



STS-3

STS-3
Air-to-air views of STS-3 launch from T-38 chase aircraft
Credit: NASA


First and only landing by a shuttle at White Sands, New Mexico, after weather at Edwards did not permit landing there.

AKA: Columbia;OSS-1. Launched: 1982-03-22. Returned: 1982-03-30. Number crew: 2 . Duration: 8.00 days.

Payloads included Office of Space Science (OSS) experiments, Monodisperse Latex Reactor (MLR), Electrophoresis Verification Test (EEVT), Plant Lignification Experiment.

Orbits of Earth: 129. Distance traveled: 7,081,113 km. Orbiter Liftoff Mass: 106,782 kg. Orbiter Mass at Landing: 93,924 kg. Payload to Orbit: 10,301 kg. Payload Returned: 10,301 kg. Landed at: Runway 17 dry lake bed at White Sands Missile Rang. Landing Speed: 407 kph. Touchdown miss distance: 332 m. Landing Rollout: 4,187 m.

NASA Official Mission Narrative

Mission Name: STS-3 (3)
COLUMBIA (3)
Pad 39-A (15)
3rd Shuttle mission
3rd Flight OV-102
Extended mission
2nd RMS Mission
1st White Sands landing

Crew:
Jack R. Lousma (2), Commander
C. Gordon Fullerton (1), Pilot Backup

Crew: (after STS-3, backup crews were no longer named)
Thomas K. Mattingly (1), Commander
Henry W. Hartsfield (0), Jr., Pilot

Milestones:
OPF - Nov. 26,1981
VAB - Feb. 3, 1982
PAD - Feb, 16, 1982

Payload:
OSS-1,DFI(3),MLR,EEVT,HBT,SSIP(x1),GAS(x1)
Mission Objectives:
Demonstrate safe re-launch and safe return of the orbiter and crew. Verify the combined performance of the entire shuttle vehicle - orbiter, solid rocket boosters and external tank.
Payloads included the 8,740lb Office of Space Science (OSS-1) Pallet consisting of the Plant Lignification Experiment, the Plasma Diagnostic Package (PDP), the Vehical Charging and Potential (VCAP) experiment, the Space Shuttle Induced Atmosphere experiment, the Thermal Canister experiment, the Solar Flare X-Ray Polarimeter, the Solar Ultraviolet and Spectral Irradiance Monitor (SUSIM), the Contamination Monitor Package and the Foil Microabrasion Package. Also in the payload bay was the 11,048lb Development Flight Instrumentation (DFI) Pallet and the 448lb Aerodynamic Coefficient Identification Package (ACIP).
The crew compartment housed the Monodisperse Latex Reactor (MLR) experiment and the Heflex Bioengineering Test (HBT) experiment.

Launch:
March 22, 1982, 11:00:00 a.m. EST. Launch delayed one hour due to failure of heater on nitrogen gas ground support line. Launch Weight: 235,415 lbs.
Orbit:
Altitude: 147nm
Inclination: 38.0 degrees
Orbits: 130
Duration: Eight days, zero hours. Four minutes, 46 seconds.
Distance: 3,334,904 miles

Hardware:
SRB: BI-003
SRM: 003SW(SPM)
ET : 4/SWT-3
MLP: 1
SSME-1: SN-2007
SSME-2: SN-2006
SSME-3: SN-2005

Landing:
March 30, 1982,9:04:46 a.m. MST, Runway 17, Northrup Strip, White Sands, N.M. Rollout distance: 13,737 feet. Rollout time: 84 seconds. Landing site changed from Edwards to White Sands due to wet conditions on Edwards dry lake bed landing site. High winds at White Sands resulted in one day extension of mission, Some brake damage upon landing and dust storm caused extensive contamination of orbiter. Orbiter returned to KSC April 6, 1982. Landing Weight: 207,072 lbs.

Mission Highlights:
Testing continued of Space Shuttle systems for qualification for operational flights. Testing of remote manipulator system and measurements of thermal response of orbiter in various attitudes to sun conducted. Get Away Special test canister and Spacelab pallet-mounted experiments for NASA's Office of Space Science- 1 (OSS-1) carried in payload bay. 0SS-1 obtained data on near- Earth space environment, including contamination (gases, dust, etc.) introduced into space by orbiter itself. Other experiments: Monodisperse Latex Reactor (MLR), Electrophoresis Equipment Verification Test (EEVT), Heflex Bioengineering Test (HBT) and first Shuttle Student Involvement Program (SSIP) experiment. Problems encountered: space sickness, malfunctioning toilet, thermostat difficulty and unexplained static interfering with crew sleep. Auxiliary power unit registered overheating during ascent, but functioned properly during descent. Three communications links lost.


More at: STS-3.


Family: Manned spaceflight. People: Fullerton, Lousma. Country: USA. Spacecraft: Columbia. Projects: STS. Launch Sites: Cape Canaveral. Agency: NASA, NASA Houston.


Photo Gallery





STS-3 STS-3MOCR activity during STS-3 missionCredit: NASA


STS-3 STS-3Pilot Fullerton dons anti-g and ejection escape suit (EES) on middeckCredit: NASA


STS-3 STS-3Night firing of orbiter Columbia's thrustersCredit: NASA


STS-3 STS-3Pilot Fullerton plans menu as packaged food and beverages float around himCredit: NASA


STS-3 STS-3Commander Lousma examines Insect Flight Motion StudyCredit: NASA


STS-3 STS-3View of the Columbia's aft section while over Morocco's Atlantic CoastCredit: NASA


STS-3 STS-3Pilot Fullerton eats on middeckCredit: NASA


STS-3 STS-3Payload bay, Northern Persian Gulf RegionCredit: NASA


STS-3 STS-3Los Angeles, CA.Credit: NASA


STS-3 STS-3Commander Lousma is surrounded by a week's worth of trash on the middeckCredit: NASA


STS-3 STS-3Commander Lousma sleeps on aft flight deckCredit: NASA


STS-3 STS-3Earth Limb and Hurricane Clouds over Open Ocean, Location UnknownCredit: NASA


STS-3 STS-3Air-to-air coverage of orbiter inspection during its descentCredit: NASA


STS-3 STS-3EMU TV system testCredit: NASA



1982 March 22 - . 16:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP1. LV Family: Shuttle. Launch Vehicle: Space Shuttle.


1982 March 23 - .


1982 March 24 - .


1982 March 25 - .


1982 March 26 - .


1982 March 27 - .


1982 March 28 - .


1982 March 29 - .


1982 March 30 - .



Back to top of page


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z


© 1997-2019 Mark Wade - Contact
© / Conditions for Use