STS-43

STS-43

Atlantis deploying TDRS-E
Mission type Satellite deployment
Technology
Operator NASA
COSPAR ID 1991-054A
SATCAT № 21638
Mission duration 8 days, 21 hours, 21 minutes, 25 seconds
Distance travelled 5,955,217 kilometers (3,700,400 mi)
Orbits completed 142
Spacecraft properties
Spacecraft Space Shuttle Atlantis
Landing mass 89,239 kilograms (196,738 lb)
Payload mass 21,067 kilograms (46,445 lb)
Crew
Crew size 5
Members John E. Blaha
Michael A. Baker
Shannon W. Lucid
G. David Low
James C. Adamson
Start of mission
Launch date 2 August 1991, 15:01:59 (1991-08-02UTC15:01:59Z) UTC
Launch site Kennedy LC-39A
End of mission
Landing date 11 August 1991, 12:23:25 (1991-08-11UTC12:23:26Z) UTC
Landing site Kennedy SLF Runway 15
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee 301 kilometres (187 mi)
Apogee 306 kilometres (190 mi)
Inclination 28.45 degrees
Period 90.6 min


Left to right: Lucid, Adamson, Blaha, Low, Baker

Space Shuttle program
← STS-40 STS-48 →

STS-43, the ninth mission for Space Shuttle Atlantis, was a nine-day mission whose primary goal was launching the fourth Tracking and Data Relay Satellite, TDRS-E. The flight also tested an advanced heatpipe radiator for potential use on the then-future space station and conducted a variety of medical and materials science investigations.

Crew

Position Astronaut
Commander John E. Blaha
Third spaceflight
Pilot Michael A. Baker
First spaceflight
Mission Specialist 1 Shannon W. Lucid
Third spaceflight
Mission Specialist 2 G. David Low
Second spaceflight
Mission Specialist 3 James C. Adamson
Second spaceflight

Crew seating arrangements

Seat[1] Launch Landing
Seats 1–4 are on the Flight Deck. Seats 5–7 are on the Middeck.
S1 Blaha Blaha
S2 Baker Baker
S3 Lucid Adamson
S4 Low Low
S5 Adamson Lucid

Preparations and Launch

The launch took place on 2 August 1991, 11:01:59 am EDT. Launch was originally set for 23 July but was moved to 24 July to allow time to replace a faulty integrated electronics assembly that controls orbiter/external tank separation. The mission was postponed again about five hours before liftoff on 24 July due to a faulty main engine controller on the number three main engine. The controller was replaced and retested; launch was reset for 1 August. Liftoff set for 11:01 am delayed due to cabin pressure vent valve reading and postponed at 12:28 pm due to unacceptable return-to-launch site weather conditions. Launch finally occurred on 2 August 1991 without further delays. Launch weight: 117,650 kilograms (259,370 lb).

Mission Highlights

Launch of Space Shuttle Atlantis from the Kennedy Space Center.
TDRS-E deployment from STS-43.
Atlantis passes over Florida. SHARE-II is prominent on the left.
Crewmembers pose for on-orbit portrait in the middeck of Atlantis.

The primary payload, Tracking and Data Relay Satellite-5 (TDRS-5 or TDRS-E), attached to an Inertial Upper Stage (IUS), was deployed about six hours into flight, and the IUS propelled the satellite into geosynchronous orbit. TDRS-5 became the fourth member of the 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.[2]

TDRS E, which became TDRS-5 on orbit, was successfully boosted to geosynchronous orbit at more than 22,000 miles (35,400 kilometres (22,000 mi)) above Earth by two firings of the Inertial Upper Stage (IUS) booster, the last of which occurred approximately 12½ hours into the mission. TDRS then deployed its antennas and solar panels, and separation from the IUS took place less than 45 minutes later.

The TDRS network of satellites provides the vital communication link between Earth and low-orbiting spacecraft such as the Space Shuttle. Until the STS-43 deployment, there were three TDRS spacecraft on orbit above the equator: two were in the west position over the Pacific Ocean, southwest of Hawaii. TDRS-4 was in the east position over the northeast corner of Brazil. TDRS-B was lost in the Challenger accident in 1986. After STS-43, the two satellites in the west became on-orbit spares; TDRS-5, after activation, checkout and calibration, officially became the primary provider of services in the west location on 7 October 1991. It was stationed at 175 degrees west longitude.

Previously, orbiting spacecraft could communicate with Earth only when in sight of a ground tracking station – about 15 percent of each orbit. The TDRS network allows communication from 85 to 100 percent of an orbit, depending on the spacecraft's altitude.

The crew was kept busy with the operation of varied experiments during the nine-day flight. The Space Station Heat Pipe Advanced Radiator Element II (SHARE-II) experiment tested a natural cooling process for transferring thermal energy that could serve as a cooling system for Space Station Freedom. The Solid Surface Combustion Experiment provided some answers about how fire behaves in microgravity. The crew also activated other previously flown materials science experiments and participated in medical experiments in support of long-duration flights. One test showed that optical fibers could provide video and audio links between the flight deck and the payload bay.

Crew members in space and flight controllers on the ground demonstrated their ingenuity when they adapted a camera part to replace one that had not been packed for the mission.

The crew experienced some minor problems, none of them critical to the safety or success of the mission. A cooling system for Auxiliary Power Unit (APU) 2 failed to activate during an on-orbit test. APU 2 is one of three redundant systems which provide hydraulic pressurization to orbiter steering systems during entry and landing. APU 2 was still available for use in landing.

Landing: 11 August 1991, 8:23:25 am EDT, Runway 15, Kennedy Space Center, FL. 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: 88,944 kilograms (196,088 lb).

Mission insignia

The four stars on the top-left and three stars on the top-right of the insignia symbolize the flight's numerical designation in the Space Transportation System's mission sequence. The insignia is shaped to resemble an Erlenmeyer flask.

See also

References

  1. ↑ "STS-43". Spacefacts. Retrieved 26 February 2014.
  2. ↑ http://www.nasa.gov/mission_pages/shuttle/shuttlemissions/archives/sts-43.html

External links

 This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.

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