- DISCOVERY (13)
- Pad 39-A (42)
- 43rd Shuttle mission
- 13th Flight OV-103
- 5th Night landing
- John O. Creighton (3), Commander
- Kenneth S. Reightler, Jr. (1), Pilot
- James F. Buchli (4), Mission Specialist 1
- Charles D. Gemar (2), Mission Specialist 2
- Mark N. Brown (2), Mission Specialist 3
- OPF - May 6, 1991
- VAB - July 25, 1991
- PAD - Aug. 12, 1991
- UARS, AMOS(1), APM, MODE, SAM, CREAM, PARE, PGC-II-2, IPMP
Click here for Press Kit
Click here for Additional Info on STS-48
- September 12, 1991, 7:11:04 p.m. EDT. Launch delayed 14
minutes by a faulty communication link between KSC and Mission
Control in Houston. Launch Weight: 240,062 lbs.
- Altitude: 313nm
- Inclination: 57.0 degrees
- Orbits: 81
- Duration: 5 days, 8 hours, 27 minutes, 38 seconds.
- Distance: 2,193,670 miles
- SRB: BI-046
- SRM: 360L018
- ET : 42/LWT-35
- MLP : 3
- SSME-1: SN-2019
- SSME-2: SN-2031
- SSME-3: SN-2107
- September 18,1991, 12:38:42 a.m. PDT, Runway 22, Edwards AFB,
Calif. Rollout distance: 9,513 feet. Rollout time: 50 seconds.
Landed scheduled for KSC, but diverted to Edwards due to bad weather.
Orbiter returned to KSC Sept. 26,1991. Landing Weight: 192,780 lbs.
KSC Home Mission Index
Last Mission STS-43
Next Mission STS-44
- Primary payload, the Upper Atmosphere Research Satellite
(UARS), deployed on the third day of the mission. During its
planned 18-month mission, the l4,500-pound observatory will
make the most extensive study ever conducted of the Earth's
troposphere, the upper level of the planet's envelope of life-
sustaining gases which also include the protective ozone layer.
UARS has ten sensing and measuring devices: Cryogenic Limb
Array Etalon Spectrometer (CLAES); Improved Stratospheric and
Mesospheric Sounder (ISAMS); Microwave Limb Sounder (MLS);
Halogen Occultation Experiment (HALOE); High Resolution Doppler
Imager (HRDI); Wind Imaging Interferometer (WlNDII); Solar
Ultraviolet Spectral Irradiance Monitor (SUSIM); Solar/Stellar Irra-
diance Comparison Experiment (SOLSTICE); Particle Environ-
ment Monitor (PEM) and Active Cavity Radiometer Irradiance
Monitor (ACRIM II).
- Secondary payloads were: Ascent Particle Monitor (APM);
Middeck 0-Gravity Dynamics Experiment (MODE); Shuttle Activation
Monitor (SAM); Cosmic Ray Effects and Activation Monitor (CREAM);
Physiological and Anatomical Rodent Experiment (PARE); Protein Crystal
Growth II-2 (PCG II-2); Investigations into Polymer Membrane Processing
(IPMP); and the Air Force Maui Optical Site (AMOS) experiment.
Last Updated Friday June 29 11:21:02 EDT 2001
Jim Dumoulin (firstname.lastname@example.org)