Bremen (original) (raw)

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Bremen

German manufacturer of rockets and spacecraft. OHB System GmbH, Germany.

AKA: DaimlerChrysler Aerospace, Bremen (formerly ERNO);ERNO;OHB System GmbH;SSC/MBB/ERNO.

Country: Germany. Spacecraft: Spacelab, Mir, BremSat, Inspector, Safir satellite, ABRIXAS, Rubin, SAR-Lupe. Launch Vehicles: Forschungsflugkorper. Projects: STS.

1994 February 3 - . 12:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP3. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

BremSat 1 - . Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 63 kg (138 lb). Nation: Germany. Agency: Bremen, DARA. Class: Technology. Type: Re-entry test vehicle. Spacecraft: BremSat. Decay Date: 1995-02-12 . USAF Sat Cat: 22998 . COSPAR: 1994-006H. Apogee: 160 km (90 mi). Perigee: 156 km (96 mi). Inclination: 57.00 deg. Period: 87.70 min. Atomic oxygen, dust particle, microgravity, reentry experiments. .

1997 April 4 - . 19:20 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP3. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

MSL-1 Spacelab - . Payload: Spacelab Long Module 1. Nation: USA. Agency: NASA Houston. Manufacturer: Bremen. Program: Spacelab. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacelab. Decay Date: 1997-04-08 . USAF Sat Cat: 24755 . COSPAR: 1997-013xx. Apogee: 302 km (187 mi). Perigee: 298 km (185 mi). Inclination: 28.50 deg. Period: 90.50 min. Remained attached to OV-102.

1997 July 1 - . 18:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP1. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

STS-94 - . Call Sign: Columbia. Crew: Crouch, Gernhardt, Halsell, Kilrain, Linteris, Thomas, Voss, Janice. Payload: Columbia F23 / Spacelab LM Unit 1 / EDO. Mass: 115,900 kg (255,500 lb). Nation: USA. Related Persons: Crouch, Gernhardt, Halsell, Kilrain, Linteris, Thomas, Voss, Janice. Agency: NASA Houston. Manufacturer: Bremen. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-94. Spacecraft Bus: Shuttle. Spacecraft: Columbia. Duration: 15.70 days. Decay Date: 1997-07-17 . USAF Sat Cat: 24849 . COSPAR: 1997-032A. Apogee: 300 km (180 mi). Perigee: 296 km (183 mi). Inclination: 28.50 deg. Period: 90.50 min.
STS-94 was the reflight, with the same equipment and crew, of the curtailed STS-83 mission. Cargo Bay Payloads:
- MSL-1: The Microgravity Science Laboratory included the first test of the International Space Station's EXPRESS Rack. MSL-1 also contained numerous other experiment payloads to test materials and combustion processes in zero gravity.
- CRYOFD: The Cryogenic Flexible Diode (CRYOFD) heat pipe was a Hitchhiker payload.
- OARE: The Orbital Acceleration Research Experiment was a self-calibrating instrument that monitored extremely small accelerations and vibrations experienced during orbit of the Shuttle.
  In-Cabin Payloads: SAREX, MSX
  The mission this time went for its full two week duration and the crew completed the full list of experiments. The deorbit burn was on July 17, 1997 at 09:44 GMT and Columbia landed on KSC's Runway 33 at 10:46:34 GMT.
Spacelab MSL-1R - . Payload: Spacelab Long Module. Nation: USA. Agency: NASA Houston. Manufacturer: Bremen. Program: Spacelab. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacelab. Decay Date: 1997-07-17 . USAF Sat Cat: 24849 . COSPAR: 1997-032xx. Apogee: 300 km (180 mi). Perigee: 296 km (183 mi). Inclination: 28.50 deg. Period: 90.50 min. Remained attached to OV-102.

1997 August 7 - . 14:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP3. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

CRISTA - . Payload: ASTRO-SPAS. Mass: 3,230 kg (7,120 lb). Nation: Germany. Agency: DLR. Manufacturer: Bremen. Class: Earth. Type: Atmosphere satellite. Spacecraft Bus: Shuttle Attached Payloads. Spacecraft: SPAS. Decay Date: 1997-08-19 . USAF Sat Cat: 24890 . COSPAR: 1997-039B. Apogee: 296 km (183 mi). Perigee: 282 km (175 mi). Inclination: 57.00 deg. Period: 90.30 min. Recaptured August 16..

1997 October 5 - . 15:08 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.

X-Mir Inspector - . Payload: Inspector. Nation: Germany. Agency: DASA. Manufacturer: Bremen. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TM-26, STS-84 Mir NASA-4, STS-86, STS-86 Mir NASA-5. Spacecraft: Inspector. Decay Date: 1998-11-02 . USAF Sat Cat: 25100 . COSPAR: 1997-058D. Apogee: 387 km (240 mi). Perigee: 377 km (234 mi). Inclination: 51.70 deg. Period: 91.10 min.

1998 April 17 - . 18:19 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39B. Launch Platform: MLP2. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

STS-90 - . Call Sign: Columbia. Crew: Altman, Buckey, Hire, Linnehan, Pawelczyk, Searfoss, Williams, Dave. Backup Crew: Dunlap, Mukai. Payload: Columbia F25 / Spacelab LM Eurolab. Mass: 115,900 kg (255,500 lb). Nation: USA. Agency: NASA Houston. Manufacturer: Bremen. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-90. Spacecraft Bus: Shuttle. Spacecraft: Columbia. Duration: 15.91 days. Decay Date: 1998-05-03 . USAF Sat Cat: 25297 . COSPAR: 1998-022A. Apogee: 274 km (170 mi). Perigee: 247 km (153 mi). Inclination: 39.00 deg. Period: 89.70 min.
Columbia rolled out to pad 39B on March 23. Payloads:
- Spacelab transfer tunnel
- Spacelab Long Module, with Neurolab experiments for the following life science studies:
  * Chronic Recording of Otolith Nerves in Microgravity
  * Development of the Aortic Baroreflex under Conditions of Microgravity
  * Neural-Thyroid Interaction on Skeletal Isomyosin Expression in OG
  * Spatial Orientation of the Vestibulo-Ocular Reflex and Velocity Storage
  * Autonomic Neuroplasticity in Weightlessness
- Extended Duration Orbiter pallet
- Two Get Away Special beams with canisters G-197, G-467, G-772 (Colorado's COLLIDE experiment, which collided small particles into each other to simulate the formation of planets and rings).
  The Neurolab mission was managed by NASA-Johnson at Houston, unlike earlier Spacelab flights which were NASA-Marshall/Huntsville's responsibility. Landed at Kennedy Space Center May 3 1998.

1998 July 10 - . 06:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2.

SAFIR-2 - . Mass: 60 kg (132 lb). Nation: Germany. Agency: DLR. Manufacturer: Bremen. Class: Communications. Type: Civilian store-dump communications satellite. Spacecraft: Safir satellite. USAF Sat Cat: 25399 . COSPAR: 1998-043F. Apogee: 819 km (508 mi). Perigee: 815 km (506 mi). Inclination: 98.80 deg. Period: 101.20 min. Relay satellite built by OHB System of Bremen..

1999 April 28 - . 20:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

ABRIXAS - . Mass: 470 kg (1,030 lb). Nation: Germany. Agency: DLR. Manufacturer: Bremen. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: ABRIXAS. Decay Date: 2017-10-31 . USAF Sat Cat: 25721 . COSPAR: 1999-022A. Apogee: 407 km (252 mi). Perigee: 393 km (244 mi). Inclination: 48.45 deg. Period: 92.57 min. X-ray astronomy satellite with the mission to carry out an all-sky survey in the 1-10 keV band. The satellite's battery failed and contact was lost on May 1..

2000 July 15 - . 12:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Rubin - . Nation: Germany. Agency: RVSN. Manufacturer: Bremen. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rubin. Decay Date: 2001-08-30 . USAF Sat Cat: 26406 . COSPAR: 2000-039C. Apogee: 463 km (288 mi). Perigee: 411 km (255 mi). Inclination: 87.26 deg. Period: 93.23 min. Rubin was a microsatellite to measure launch vehicle parameters developed by OHB and students of the Hochschule Bremen. Rubin remained attached to the payload adapter of the Kosmos-3M final stage..

2002 November 28 - . 06:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Rubin-3-DSI - . Mass: 80 kg (176 lb). Nation: Russia. Agency: NCST. Manufacturer: AKO Polyot, Bremen. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rubin. USAF Sat Cat: 27561 . COSPAR: 2002-054C. Apogee: 748 km (464 mi). Perigee: 687 km (426 mi). Inclination: 98.20 deg. Period: 99.10 min.
Delayed from September 12, October 29. Rubin-3-DSI, with a mass of 45 kg, was built by PO Polyot of Omsk (builders of the Kosmos-3M) and OHB System of Bremen. It remained attached to the booster final stage and measured the launch vehicle environment and performance

2002 December 20 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.

Rubin 2 - . Mass: 45 kg (99 lb). Nation: Germany. Agency: Makeyev bureau. Manufacturer: Bremen. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 27609 . COSPAR: 2002-058E. Apogee: 645 km (400 mi). Perigee: 639 km (397 mi). Inclination: 64.60 deg. Period: 97.60 min. Messaging technology satellite..

2006 December 19 - . 14:03 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

SAR-Lupe 1 - . Mass: 770 kg (1,690 lb). Nation: Germany. Agency: BWB. Manufacturer: Bremen. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: SAR-Lupe. USAF Sat Cat: 29658 . COSPAR: 2006-060A. Apogee: 506 km (314 mi). Perigee: 467 km (290 mi). Inclination: 98.20 deg. Period: 94.30 min. First of five planned German military surveillance satellites using synthetic aperture radar for target coverage at night and in all weathers. Orbital plane ascending node 143 deg..

2007 July 2 - . 19:38 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

SAR-Lupe 2 - . Mass: 770 kg (1,690 lb). Nation: Germany. Agency: BWB. Manufacturer: Bremen. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: SAR-Lupe. USAF Sat Cat: 31797 . COSPAR: 2007-030A. Apogee: 508 km (315 mi). Perigee: 470 km (290 mi). Inclination: 98.20 deg. Period: 94.40 min. Second of five planned German military surveillance satellites using synthetic aperture radar for target coverage at night and in all weathers. Orbital plane ascending node 208 deg..

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