STS-51

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This article is about the Space Shuttle mission STS-51, flown in 1993. For the missions in the early 1980s that used designations STS-51-A through to STS-51-L, see STS-51 (disambiguation).
STS-51
1993 s51 IMAX view of Discovery from Spas.JPG
Discovery in orbit, seen from the SPAS astronomy platform
Mission type Satellite deployment
Astronomy
Operator NASA
COSPAR ID 1993-058A
SATCAT № 22795
Mission duration 9 days, 20 hours, 11 minutes, 11 seconds
Distance travelled 6,608,628 kilometers (4,106,411 mi)
Orbits completed 157
Spacecraft properties
Spacecraft Space Shuttle Discovery
Landing mass 92,371 kilograms (203,643 lb)
Payload mass 18,947 kilograms (41,771 lb)
Crew
Crew size 5
Members Frank L. Culbertson, Jr.
William F. Readdy
James H. Newman
Daniel W. Bursch
Carl E. Walz
Start of mission
Launch date 12 September 1993, 11:45 (1993-09-12UTC11:45Z) UTC
Launch site Kennedy LC-39B
End of mission
Landing date 22 September 1993, 07:56 (1993-09-22UTC07:57Z) UTC
Landing site Kennedy SLF Runway 15
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee 300 kilometres (190 mi)
Apogee 308 kilometres (191 mi)
Inclination 28.45 degrees
Period 90.6 min

STS-51 patch.svg STS-51-crew.jpg
Left to right: Culbertson, Bursch, Walz, Readdy, Newman


Space Shuttle program
← STS-57 STS-58

STS-51 was a Space Shuttle Discovery mission that launched the Advanced Communications Technology Satellite (ACTS) in September 1993. The flight also featured the deployment and retrieval of the SPAS-ORFEUS satellite and its IMAX camera, which captured spectacular footage of Discovery in space. A spacewalk was also performed during the mission to evaluate tools and techniques for the STS-61 Hubble Space Telescope servicing mission later that year. STS-51 was the first shuttle mission to fly a GPS receiver, a Trimble TANS Quadrex. It was mounted in an overhead window where limited field of view and signal attenuation from the glass severely impacted receiver performance.[1] (Full triple-redundant 3-string GPS would not happen until 14 years later with STS-118.)

Crew[edit]

Position Astronaut
Commander Frank L. Culbertson, Jr.
Second spaceflight
Pilot William F. Readdy
Second spaceflight
Mission Specialist 1 James H. Newman
First spaceflight
Mission Specialist 2 Daniel W. Bursch
First spaceflight
Mission Specialist 3 Carl E. Walz
First spaceflight

Spacewalks[edit]

  • Newman and Walz – EVA 1
  • EVA 1 Start: 16 September 1993 – 08:40 UTC
  • EVA 1 End: 16 – 15 September:45 UTC
  • Duration: 7 hours, 05 minutes

Launch Preparations[edit]

Launch as seen from the RSS.

STS-51 was notable for having been scrubbed three times on the launchpad, each time after the crew had boarded the spacecraft:[2]

  • On 17 July 1993, the launch was scrubbed on the pad due to a flaw in the pyrotechnic initiator controller that triggers the release of the solid rocket boosters from the mobile launcher platform.
  • On 24 July 1993, problems with a hydraulic power unit in one of the solid rocket boosters caused another scrub on the pad. Because of the Perseid meteor shower, the next launch window did not open until the second week of August.
  • On 12 August 1993, the count reached the T−3 second mark, at which point the Space Shuttle Main Engine (SSMEs) had ignited. A shutdown was then triggered by faulty fuel flow sensors in one of the SSMEs.
  • STS-51 successfully launched on 12 September 1993.


Advanced Communications Technology Satellite (ACTS)[edit]

ACTS deployment.
ACTS heads for Geostationary Orbit.

The Advanced Communications Technology Satellite was deployed on flight day 1. This satellite served as a test bed for advanced experimental communications satellite concepts and technology. Its Transfer Orbit Stage (TOS) upper stage fired on time 45 minutes after deployment and boosted the satellite to geosynchronous altitude on the first day of the mission.

The first attempt to deploy ACTS was delayed by the crew when two-way communications were lost with Mission Control about 30 minutes before the deploy time. Flight controllers could receive telemetry and voice communications from Discovery, however the crew could not receive communications from the ground. The crew waived off the 2:43 pm CDT deploy when they did not receive a "go" from Mission Control as called for in preflight plans made for just such an occurrence.

After the waive off of deploy, the crew changed the shuttle's S-Band communications system to a lower frequency and restored two-way communications with the ground. The two-way communications had been lost for a total of about 45 minutes. After consulting the crew, flight controllers began immediately planning for the second, and ultimately successful deploy.

During the deployment on 12 September, two Super*Zip explosive cords in the Airborne Support Equipment cradle (ASE) designed to release the spacecraft, one primary and the other a backup, simultaneously detonated. This caused minor tears in two dozen insulation blankets mounted on the bulkhead between the payload bay and the AFT near the #3 APU. The ASE ring holding the TOS was damaged as well, and ejected debris was visible as the stack moved away from the orbiter.

The Advanced Communications Technology Satellite (ACTS), a significant activity of the NASA Space Communications Program, provided for the development and flight test of high-risk, advanced communications satellite technology. Using multiple spot beam antennas and advanced on-board switching and processing systems, ACTS pioneered new initiatives in communications satellite technology. NASA Glenn Research Center was responsible for the development, management, and operation of ACTS as part of a long legacy of experimental communications satellites.

After fulfilling its original mission, the spacecraft continued operations through a partnership between the space agency and a nonprofit consortium. It was shut down 28 April 2004 after funding dried up. The satellite was put into a flat spin with its solar array edges facing the sun, preventing it from ever being restarted. The spacecraft was moved to its final resting place at 105.2 degrees west longitude – where it poses minimal risk to other satellites – after NASA concluded in 2000 that it probably lacked the fuel to move to a higher graveyard orbit. Nevertheless, ACTS should not re-enter the atmosphere for thousands of years, according to Richard Krawczyk, the ACTS operations manager at Glenn Research Center.[3]

SPAS-ORFEUS[edit]

The ORFEUS\SPAS platform is captured by the RMS.

Another payload on this mission was the Orbiting Retrievable Far and Extreme Ultraviolet Spectrometer (ORFEUS) telescope mounted on the Shuttle Pallet Satellite (SPAS) payload carrier. ORFEUS was designed to provide information on how stars are born and how they die, while studying gaseous interstellar clouds. Also in the cargo bay was the Limited Duration Space Environment Candidate Materials Exposure (LDCE) experiment.

MBB (Messerschmitt-Bölkow-Blohm) began development of the SPAS carrier (flown previously on STS-7, STS-41B, and STS-39) in 1986 into a free-flying astronomical platform. The DARA/NASA agreement called for four co-operative science missions, with DARA providing the satellite, NASA the Shuttle launch and deployment/retrieval services, and the two parties sharing the science instruments. NASA provided the Shuttle free of charge, in return for access to data and the inclusion of US experiments. ORFEUS, the Orbiting and Retrievable Far/Extreme UV Spectrometer, designed to measure radiation between 400–1,280 angstroms, was released at 14.06 GMT 13 September 1993, and was retrieved at 11.50 GMT 19 September 1993. Science contributions came from the University of Tübingen, Sternwarte Heidelberg, University of California, Berkeley and Princeton University (IMPAS). ORFEUS' telescope was fabricated by Kayser-Threde in Germany; France's REOSC provided the 1 m f/2.5 mirror. The separate 950-1,150 Å IMAPS Interstellar Medium Absorption Profile Spectrograph added to the observations of hot galactic objects and the interstellar medium at high spectral resolution (240,000). Other payloads were DLR's Surface Effective Sample Monitor and Canada's IMAX Cargo Bay Camera, which was used to film Discovery in orbit for the IMAX film Destiny in Space. A portion of this footage was also included in Space Station 3D. This was the fourth flight of the SPAS platform, of a total of seven during the space shuttle program. The SPAS-ORFEUS version was reflown on mission STS-80 in 1996.

EVA[edit]

Walz during the EVA.

On Thursday, 16 September 1993, spacewalkers Jim Newman and Carl Walz performed an EVA designed to evaluate tools, tethers and a foot restraint platform. Their findings reassured the designers and planners of the Hubble Space Telescope servicing flight that their preparations were sound. This was the third and final shuttle mission to include a preparatory EVA in response to the weaknesses in EVA training exposed by the STS-49 mission. The new equipment tested during the extensive spacewalk would later be required for the December 1993 Hubble Space Telescope servicing mission, and was only part of the objectives of the spacewalk, with Newman and Walz fulfilling the other goals as they explained at length to Mission Control the differences they perceived between work in orbit and ground training. The two EVA crewmen were ahead of schedule much of the day, and completed more tasks than originally planned. As the two astronauts were cleaning up, a balky tool box lid slowed them down when they had to pry it free and close it for Discovery'’s trip home. The toolbox lid stretched the spacewalk by about 45 minutes over what had been planned, with Newman and Walz logging a total seven hours, five minutes and 28 seconds of time outside the vehicle. This was the 112th EVA performed in the history of human spaceflight.

Secondary Experiments[edit]

In-cabin payloads included the Air Force Maui Optical Site (AMOS) Auroral Photography Experiment-B (APE-B), Commercial Protein Crystal Growth (CPCG), Chromosome and Plant Cell Division in Space (CHROMEX), High Resolution Shuttle Glow Spectroscopy-A (HRSGS-A), IMAX, Investigations into Polymer Membrane Processing (IPMP) and the Radiation Monitoring Equipment-III (RME-III) experiment. The Investigation into Polymer Membrane Processing, or IPMP, is designed to research the mixing of various solvent systems in the absence of convection found on Earth in hopes of controlling the porosity of various polymer membranes. RME measures gamma ray, electron, neutron and proton radiation levels in the crew cabin throughout the flight.

On board, Mission Specialist Jim Newman donned a special visor to perform a medical experiment testing vision in weightlessness as part of investigations into how vision compensates for the inner ear's lack of balance in space. Newman also successfully tested a Global Positioning System receiver flying aboard Discovery as an evaluation of using such equipment to supplement the shuttle's navigation. Also, in a precursor of space station operations, one of Discovery’s fuel cells was turned off and restarted.

In another medical evaluation, Commander Frank Culbertson and Mission Specialist Dan Bursch rode a stationary bike on Discovery’s lower deck as part of a continuing study of using exercise to counteract the effects of weightlessness on the body. The crew also powered up an experiment that looks at improving membrane filters in weightlessness and checked on another experiment that has been running well studying the effects of microgravity on plant cells.

Astronauts Carl Walz and Jim Newman operated the experiments designed to study the glowing effect, one a spectrometer that records the effect on film in fine detail and another that records the effect on still photographs. The experiments are hoped to provide information about just what types of gases – in addition to atomic oxygen – create the glow. The information on kinds of gases in the extreme reaches of the atmosphere may be coupled with the materials exposure experiment in the cargo bay to assist with the design and construction of future spacecraft.

Mission insignia[edit]

The five white stars and one yellow star of the insignia symbolize the flight's numerical designation in the Space Transportation System's mission sequence. The insignia also depicts the triangular SPAS-ORFEUS on the right.

See also[edit]

References[edit]

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

  1. ^ "Analysis of the First Successful Flight of GPS Abroad the Space Shuttle". NAVAL POSTGRADUATE SCHOOL. Retrieved 17 November 2009. 
  2. ^ "STS 51 (57)". NASA. Retrieved 29 March 2008. 
  3. ^ [1][dead link]

External links[edit]