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STS-69

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STS-69
Endeavour'sCanadarm grapples the Wake Shield Facility, prior to its deployment
NamesSpace Transportation System-69
Mission typeResearch
OperatorNASA
COSPAR ID1995-048AEdit this at Wikidata
SATCATno.23667
Mission duration10 days, 20 hours, 29 minutes, 56 seconds
Distance travelled7,200,000 kilometres (4,500,000 mi)
Orbits completed171
Spacecraft properties
SpacecraftSpace ShuttleEndeavour
Payload mass11,499 kg (25,351 lb)
Crew
Crew size5
Members
Start of mission
Launch date7 September 1995, 15:09:00(1995-09-07UTC15:09Z)UTC[1]
Launch siteKennedy,LC-39A
End of mission
Landing date18 September 1995, 11:38:56(1995-09-18UTC11:38:57Z)UTC[1]
Landing siteKennedy,SLF Runway 33
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude321 kilometres (199 mi)
Apogee altitude321 kilometres (199 mi)
Inclination28.4 degrees
Period91.4 min

STS-69 mission patch

Left to right – Seated: Cockrell, Walker; Standing: Gernhardt, Newman, Voss
←STS-70(70)
STS-73(72) →

STS-69was aSpace ShuttleEndeavourmission, and the second flight of theWake Shield Facility(WSF).[2]The mission launched fromKennedy Space Center,Florida on 7 September 1995. It was the 100th successful crewed NASA spaceflight[citation needed],not including X-15 flights.

Crew

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Position Astronaut
Commander David M. Walker[3]
Fourth and last spaceflight
Pilot Kenneth Cockrell[3]
Second spaceflight
Mission Specialist 1 James S. Voss[3]
Third spaceflight
Mission Specialist 2
Flight Engineer 		James H. Newman[3]
Second spaceflight
Mission Specialist 3 Michael L. Gernhardt[3]
First spaceflight

Spacewalks

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EVA 1 – Voss and Gernhardt[1]
  • EVA 1 Start:16 September 1995 – 08:20 UTC
  • EVA 1 End:16 September 1995 – 15:06 UTC
  • Duration:6 hours, 46 minutes

Crew seat assignments

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Seat[4] Launch Landing
Seats 1–4 are on the flight deck.
Seats 5–7 are on the mid-deck.
1 Walker
2 Cockrell
3 Voss Gernhardt
4 Newman
5 Gernhardt Voss
6 Unused
7 Unused

Mission highlights

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The pale blue Earth serves as a backdrop for astronautMichael Gernhardt,who is attached to the ShuttleEndeavour's robot arm during a spacewalk on the STS-69 mission in 1995. Unlike earlier spacewalking astronauts, Gernhardt was able to use an electronic cuff checklist, a prototype developed for the assembly of the International Space Station.

The 11-day mission was the second flight of theWake Shield Facility(WSF), a saucer-shaped satellite that was to fly free of the Shuttle for several days. The purpose of the WSF was togrow thin filmsin a near perfect vacuum created by the wake of the satellite as it moved through space.[1]The crew also deployed and retrieved the Spartan 201 astronomy satellite, performed a six-hour spacewalk to test assembly techniques for theinternational Space Stationand tested thermal improvements made tospacesuitsused during space walks.

The Spartan 201 free-flyer made its third flight aboard the Shuttle. The Spartan 201 mission was a scientific research effort aimed at the investigation of the interaction between the Sun and its outflowing wind of charged particles. Spartan's goal was to study the outer atmosphere of the Sun and its transition into the solar wind that constantly flows past the Earth.[5]

STS-69 saw the first flight of theInternational Extreme Ultraviolet Hitchhiker(IEH-1), the first of five planned flights to measure and monitor long-term variations in the magnitude of absolute extreme ultraviolet (EUV) flux coming from the Sun, and to study EUV emissions from the plasma torus system around Jupiter originating from its moon Io.[2]

Also aboardEndeavourwere the combined Capillary Pumped Loop-2[6]/Gas Bridge Assembly[7](CAPL-2/GBA) payload. This experiment consisted of the CAPL-2 Hitchhiker payload designed as an in-orbit microgravity demonstration of a cooling system planned for the Earth Observing System Program and the Thermal Energy Storage-2 payload, part of an effort to develop advanced energy generation techniques. Also a part of this payload were severalGetaway Special(GAS) experiments which investigated areas such as the interaction of spacecraft attitude and orbit control systems with spacecraft structures, fluid-filled beams as structural dampers in space and the effects of smoldering combustion in a long-term microgravity environment.

Another payload flown with a connection to the development of the Space Station was theElectrolysisPerformance Improvement Concept Study (EPICS). Supply of oxygen and hydrogen by electrolyzing water in space plays an important role in meeting NASA's needs and goals for future space missions. On-board generation of oxygen was expected to reduce the annual resupply requirement for the Space Station by approximately 5,400 kilograms (11,900 lb).

Other payloads aboard were the National Institutes of Health- Cells-4 (NIH-C4) experiment that investigatesbone lossduring space flight; the Biological Research in Canister-6 (BRIC-6) that studies the gravity-sensing mechanism within mammalian cells. Also flying were two commercial experiments. (CMIX-4) whose objectives included analysis of cell change in microgravity along with studies of neuro-muscular development disorders and the Commercial Generic Bioprocessing Apparatus-7 (CGBA-7). CGBA was a secondary payload that served as an incubator and data collection point for experiments in pharmaceuticals testing and biomedicine, bioprocessing and biotechnology, agriculture and the environment.[8]

The Thermal Energy Storage (TES-2) experiment was also part of the CAPL-2/GBA-6. The TES-2 payload was designed to provide data for understanding the long-duration behavior of thermal energy storage fluoride salts that undergo repeated melting and freezing in microgravity. The TES-2 payload was designed to study the microgravity behavior of voids inlithium fluoride–calcium fluorideeutectic,a thermal energy storage salt. Data from this experiment would validate a computer code called TESSIM,[9]useful for the analysis of heat receivers in advanced solar dynamic power system designs.

See also

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References

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  1. ^abcdSwan, Bobbie Gail; Harsh, George; Ong, A. Y.; Albjerg, M.; Burns, F. T. Jr. (1 December 1995)."STS-69 Space Shuttle Mission Report"(PDF).NTRS - NASA Technical Reports Server.Houston, Texas:NASA.Archived(PDF)from the original on 25 April 2021.Retrieved25 April2021.
  2. ^abRyba, Jeanne (1 April 2010)."STS-69".Space Shuttle.Archivedfrom the original on 25 April 2021.Retrieved25 April2021.
  3. ^abcdeCampion, Ed; Navias, Rob; Buckingham, Bruce; Malone, June; Martin, Cam; Cast, Jim; Savage, Don; Isbell, Doug; Braukus, Mike; Jones, Tammy (1995)."STS-69 Press Kit"(TXT).NASA News.NASA.Archivedfrom the original on 25 April 2021.Retrieved25 April2021.
  4. ^"STS-69".Spacefacts.Retrieved29 July2024.
  5. ^Schroeder, ChristineA.; Schutz, Bob E. (1 May 1996)."Performance Assessment of Two GPS Receivers on Space Shuttle"(PDF).NTRS – NASA Technical Reports Server.University of Texas at Austin,NASA.Archived fromthe original(PDF)on 25 April 2021.Retrieved25 April2021.
  6. ^Hallinan, K. P.; Allen, J. S. (1 March 1999)."Comments on the Operation of Capillary Pumped Loop Devices in Low Gravity"(PDF).NTRS – NASA Technical Reports Server.University of Dayton, Ohio,NASA.Archived(PDF)from the original on 25 April 2021.Retrieved25 April2021.
  7. ^Ottenstein, Laura; Butler, Dan; Ku, Jentung; Cheung, Kwok; Baldauff, Robert; Hoang, Triem (1 January 2002)."Flight Testing of the Capillary Pumped Loop 3 Experiment"(PDF).NTRS – NASA Technical Reports Server.NASA,United States Naval Research Laboratory,TTH Research.Archived(PDF)from the original on 25 April 2021.Retrieved25 April2021.
  8. ^Chowdhury, Abul A. (10 June 2010)."STS-69".Life Sciences Data Archive.NASA.Archived fromthe originalon 25 April 2021.Retrieved25 April2021.
  9. ^Lewis Research Center(1 March 1996)."Research and Technology 1995"(PDF).NTRS – NASA Technical Reports Server.Brook Park, Ohio:NASA.pp. 113–114.Archived(PDF)from the original on 25 April 2021.Retrieved25 April2021.
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