2 August 1991 15:07 GMT. Landing Date: 1991-08-11 12:28:37. Flight Time: 8.89 days. Flight Up: STS-43. Flight Back: STS-43. Call Sign: Atlantis. Crew: Adamson, Baker Mike, Blaha, Low, Lucid. Program: STS. Manned five crew. Deployed TDRS 5 satellite. Payloads: Tracking and Data Relay Satellite (TDRS)-E/lnertial Upper Stage (lUS), Space Station Heatpipe Advanced Radiator Element (SHARE)-ll, Shuttle Solar Backscatter Ultraviolet (SSBUV) instrument 03, Optical Communications Through the Shuttle Window (OCTW), Air Force Maui Optical Site (AMOS) Calibration Test, Auroral Photography Experiment (APE)-B, Bioserve-lnstrumentation Technology Associates Materials Dispersion Apparatus (BlMDA)-02, Investigations Into Polymer Membrane Processing (IPMP)-03, Protein Crystal Growth Ill Block Il, Space Acceleration Measure-ment System (SAMS), Solid Surface Combustion Experiment (SSCE)-02, Tank Pressure Control Experiment (TPCE). Orbits of Earth: 142. Distance traveled: 5,955,216 km. Orbiter Liftoff Mass: 117,653 kg. Orbiter Mass at Landing: 89,235 kg. Payload to Orbit: 21,265 kg. Payload Returned: 4,192 kg. Landed at: Runway 15 at Kennedy Space Center, Florida. Landing Speed: 376 kph. Touchdown miss distance: 605 m. Landing Rollout: 3,014 m.
NASA Official Mission NarrativeMission Name: STS-43 (42) Atlantis (9) Pad 39-A (41) 42nd Shuttle mission 9th Flight OV-104 Scheduled KSC landing 8th KSC landing Crew: John E. Blaha (3), Commander Michael A. Baker (1), Pilot Shannon W. Lucid (3), Mission Specialist 1 James C. Adamson (2), Mission Specialist2 G. David Low (2), Mission Specialist 3 Milestones: OPF - April 19,1991 VAB - June 19,1991 PAD - June 25,1991 Payload: TDRS-E,SSBUV-03,SHARE-II,OCTW-01,TPCE Mission Objectives: Launch: August 2,1991, 11:01:59 a.m. EDT. Launch originally set for July 23, but was moved to July 24 to allow time to replace a faulty integrated electronics assembly that controls orbiter/external tank separation. Mission postponed again about five hours before liftoff on July 24 due to a faulty main engine controller on number three main engine. Controller replaced and retested; launch reset for Aug. 1. Liftoff set for 11:01 a.m. delayed due to cabin pressure vent valve reading and postponed at 12:28 p.m. due to unacceptable return-to-launch site weather conditions. Launch reset for Aug. 2. Launch Weight: 259,374 lbs. Orbit: Altitude: 174nm Inclination: 28.45 degrees Orbits: 142 Duration: 8 days, 21 hours, 21 minutes, 25 seconds. Distance: 3,700,400 miles Hardware: SRB: BI-045 SRM: 360L017 ET : 47/LWT-40 MLP : 1 SSME-1: SN-2024 SSME-2: SN-2012 SSME-3: SN-2028 Landing: August 11, 1991, 8:23:25 a.m. EDT, Runway 15, Kennedy Space Center, Fla. Rollout distance: 9,890 feet. Rollout time: 60 seconds. First landing scheduled at KSC since 61-C in January 1986 (which was diverted to Edwards). Landing Weight: 196,088 lbs. Mission Highlights: Primary payload, Tracking and Data Relay Satellite-5 (TDRS-5) attached to an inertial Upper Stage (I US), deployed about six hours into flight, and IUS propelled satellite into geosynchronous orbit; TDRS-5 becomes fourth member of orbiting TDRS cluster. Secondary payloads were Space Station Heat Pipe Advanced Radiator Element II (SHARE II); Shuttle Solar Backscatter Ultra-Violet (SSBUV) instrument; Tank Pressure Control Equipment (TPCE) and Optical Communications Through Windows (OCTW). Other experiments included Auroral Photography Experiment (APE-B) Protein Crystal Growth Ill (PCG Ill); Bioserve / Instrumentation Technology Associates Materials Dispersion Apparatus (BIMDA); Investigations Into Polymer Membrane Processing (IPMP); Space Acceleration Measurement System (SAMS); Solid Surface Combustion Experiment (SSCE); Ultraviolet Plume imager (UVPI); and the Air Force Maui Optical Site (AMOS) experiment. STS-43 Chronology - 1991 Aug 2 - STS-43 Crew: Adamson, Baker Mike, Blaha, Low, Lucid. Spacecraft: Atlantis. Payload: Atlantis F09 / TDRS 5 [IUS]. Mass: 21,265 kg (46,881 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle. Duration: 8.89 days. Perigee: 301 km (187 mi). Apogee: 306 km (190 mi). Inclination: 28.50 deg. Period: 90.60 min.
Manned five crew. Deployed TDRS 5 satellite. Payloads: Tracking and Data Relay Satellite (TDRS)-E/lnertial Upper Stage (lUS), Space Station Heatpipe Advanced Radiator Element (SHARE)-ll, Shuttle Solar Backscatter Ultraviolet (SSBUV) instrument 03, Optical Communications Through the Shuttle Window (OCTW), Air Force Maui Optical Site (AMOS) Calibration Test, Auroral Photography Experiment (APE)-B, Bioserve-lnstrumentation Technology Associates Materials Dispersion Apparatus (BlMDA)-02, Investigations Into Polymer Membrane Processing (IPMP)-03, Protein Crystal Growth Ill Block Il, Space Acceleration Measure-ment System (SAMS), Solid Surface Combustion Experiment (SSCE)-02, Tank Pressure Control Experiment (TPCE).
Bibliography and Further Reading
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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