- STS-32
Infobox Space mission
mission_name = STS-32
insignia = STS-32 patch.png
shuttle = Columbia
launch_pad = 39-A
launch =January 9 ,1990 , 7:35:00 a.m. EST
landing =January 20 ,1990 , 1:35:37 a.m. PST,Edwards Air Force Base
duration = 10/21:00:36
altitude = 178 nautical miles (330 km)
inclination = 28.5 degrees
orbits = 172
distance = 4,509,972 miles (7,258,096 km)
crew_photo = STS-32 crew.jpg
crew_caption = Clockwise from top left: Ivins, Low, Dunbar, Wetherbee, Brandenstein.
previous =STS-33
next =STS-36 STS-32 is the 33rd launch of the
Space Shuttle and the 9th launch of Space Shuttle "Columbia". It marked the first time Pad A atKennedy Space Center 's Complex 39 was used for a launch since the 61-C mission onJanuary 12 ,1986 . It was also the first use ofMobile Launcher Platform No. 3 (MLP-3) in the Space Shuttle program, and one of the longest Shuttle missions at 10 days. Before STS-32, the only mission of the same duration had beenSTS-9 in1983 , which was the firstSpacelab mission and also on "Columbia". STS-32 executed the third night landing of the program.Crew
"(total flights to date in parentheses)"
* Daniel C. Brandenstein (3), Commander
* James D. Wetherbee (1), Pilot
* Bonnie J. Dunbar (2), Mission Specialist 1
*G. David Low (1), Mission Specialist 2
* Marsha S. Ivins (1), Mission Specialist 3Mission parameters
*
Mass :
**"Orbiter liftoff:" 116,117 kg
**"Orbiter landing:" 103,571 kg
**"Payload:" 12,014 kg
*Perigee : 296 km
*Apogee : 361 km
*Inclination : 28.5°
*Period: 91.1 minFacility preparations
Pad A was modified in preparation for the launch.
NASA made improvements to the crew emergency system and in the payload room, increased protection against freezing of the water services, installed debris traps used during propellant loading, and added more weather protection features and an umbilical to provide power, instrumentation and controls to the heaters for the solid rocket booster field joints.MLP-3, the oldest of the three Apollo-era launch structures, also underwent extensive remodeling for use with the Shuttle. Those modifications included removal of the umbilical tower, reconfiguring for three exhaust holes, and changing the electrical and mechanical ground support systems.
Mission highlights
January 9 ,1990 , 7:35:00 a.m. EST. The launch was first scheduled forDecember 18 ,1989 , but was later postponed to complete and verify modifications to Pad A. The second scheduled launch onJanuary 8 , 1990 was aborted due to weather conditions. Launch Weight: 255,994 lb (116.117 Mg). The objectives of the mission were to deploy theSYNCOM IV-F5 (also known as L.E.A.S.A.T. 5) defense communicationssatellite and retrieveNASA 'sLong Duration Exposure Facility (LDEF), whose retrieval had been delayed for 4 1/2 years by scheduling changes and an accident on 51-L. The SYNCOM IV-F5 deployed first, and a third stage Minuteman solid perigee kick motor propelled it into ageosynchronous orbit . Dunbar retrieved the LDEF on day four of the flight using the remote manipulator system. The timeliness of the retrieval had been of critical importance, because a high rate of solar flux had increased the density of the LDEF's orbital environment and accelerated its rate oforbital decay . Specialists who carefully monitored the stability of the craft's orbit had anticipated that if the LDEF was not retrieved in time, it could fall back into Earth's gravity pull and be destroyed during re-entry in February 1990.Ivins photographed the free-flying structure which held 57 science, technology and applications experiments. The 12-sided cylinder, about the size of a small bus, was then berthed in the orbiter's payload bay for return to Earth.
NASA had planned to acquire data on the crew members' exposure to long periods of
zero gravity and its effects on landing the orbiter during the extended mission. An orbiter kit was developed to allow the orbiter to operate up to 16 days in Earth orbit.The mission's exact liftoff time was determined about 12 hours before launch, using the latest tracking data on LDEF. It was flown on a 219 statute mile (352 km) orbit inclined 28.5 degrees to the
equator .The retrieval of LDEF was filmed with an
IMAX camera, and appeared in the IMAX filmDestiny in Space in 1994.The Shuttle landed on
January 20 ,1990 at 1:35:37 a.m. PST on Runway 22 ofEdwards Air Force Base inCalifornia with a landing weight of 228,335 lb (103,571 kg). The roll-out distance was 10,731 feet (3,271 m) and roll-out time was 62 seconds. The orbiter returned to KSC onJanuary 26 ,1990 .Middeck payloads
* Characterization of Neurospora Circadian Rhythms (CNCR)
* Protein Crystal Growth (PCG)
* Fluid Experiment Apparatus (FEA)
* American Flight Echocardiograph (AFE)
* Latitude / Longitude Locator (L3)
* Mesoscale Lightning Experiment(MLE)
*IMAX camera
* Air Force Maui Optical Site (AMOS) experimentMission insignia
The three stars on the left and two stars on the right of the insignia symbolize the flight's numerical designation in the Space Transportation System's mission sequence.
ee also
*
Space science
*Space shuttle
*List of space shuttle missions
*List of human spaceflights chronologically External links
* [http://science.ksc.nasa.gov/shuttle/missions/sts-32/mission-sts-32.html NASA mission information]
* [http://www.nss.org/resources/library/shuttlevideos/shuttle33.htm STS-32 Video Highlights]
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