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Space Flyer Unit

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Japanese spacecraft
Space Flyer Unit
Space Flyer Unit photographed fromEndeavour duringSTS-72 mission
Mission typeTechnology
OperatorNASDA
ISAS
NEDO
USEF
COSPAR ID1995-011AEdit this at Wikidata
SATCATno.23521
Websitewww.isas.jaxa.jp/e/enterp/missions/sfu.shtml
Mission duration10 months
Spacecraft properties
ManufacturerMitsubishi Electric
Launch mass3,846 kilograms (8,479 lb)
Landing mass3,492 kilograms (7,699 lb)
Start of mission
Launch date18 March 1995, 08:01 (1995-03-18UTC08:01Z) UTC
RocketH-II 3F
Launch siteTanegashimaYoshinobu 1
End of mission
Recovered bySpace Shuttle Endeavour
STS-72
Recovery date13 January 1996 (1996-01-14)
Landing date20 January 1996, 07:41:41 UTC
Landing siteKennedySLF Runway 15
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude470 kilometres (290 mi)
Apogee altitude492 kilometres (306 mi)
Inclination28.4 degrees
Period94.22 minutes
Epoch17 April 1995[1]
Space Flyer Unit

TheSpace Flyer Unit (宇宙実験・観測フリーフライヤ,Uchū Jikken-Kansoku Free Flyer) was a spacecraft which was launched by Japan on March 18, 1995.[2]

Technical data

[edit]
SFU exhibited in theNational Museum of Nature and Science,Tokyo.

The Space Flyer Unit was launched fromTanegashima Space Center in anH-II vehicle.[2] It carried testing materials and research data that held value to NASA. The crew ofSTS-72 aboardSpace ShuttleEndeavour retrieved the satellite on January 20, 1996, 10 months after it was launched.[2] The idea behind the implementation of the SFU was a joint effort by multiple major corporations and government agencies. The ones that were involved with the launch were theInstitute of Space and Astronautical Science,the National Space Development Agency, and theMinistry of International Trade and Industry.[3]

After the shuttle returned the SFU from space it was transported to Japan and refurbished for display at theNational Museum of Nature and Science in Tokyo.[4]

Purpose

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The original purposes behind the SFU was to[5]

  • Allow researchers better access to space research conditions.
  • Give researchers a group experimental facility.
  • Be able to reuse the SFU to save money
  • Retrieve data

Technology

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A variety of systems that were operational within the SFU had never been implemented before. Equipment on board supported aninfrared telescope, two-dimensional solar array, high voltage solar array, space plasma diagnosis, electric propulsion, material experimentation, gas dynamics, gradient heating chemicals, isothermal heating furnace and more.[6] The core system that was built into the SFU contained an octagonal aluminum truss. Inside of that were eight boxes of trapezoidal shape.[6] The SFU was connected directly to the Kagoshima Space Center.[7]

Experimentation data

[edit]
IRTS exhibited in the JAXASagamihara Campus Space Science Exploration Exchange Building

A number of various types of experiments that performed on board the SFU during its launch life cycle. Those experiments, and light data related to them are listed below.

  • Infrared Telescope in Space (IRTS) - The IRTS experiment was performed by the infrared telescope that was aboard the SFU. The intent was to produce important information into the history of the universe and structure of the milky way galaxy. The telescope had a super fluid helium cooling fan built into it to prevent it from overheating.[8]
  • 2D Array - The 2d array system was launched as a small module inside of the SFU. This experiment was deployed to show that large structures could (in fact) be built in space.[9]
  • HVSA - The Solar Array was a power source put into this system to head up multiple experiments. It is used to test the creation of "electricity" in the denseness of space from the use of technology only.[10]
  • SPDP - This was used on the SFU to test things going really fast in space. SPDP stands for (Space Plasma Diagnostic Package) and it was deployed with different sensors to check the effects of speed on the denseness of gravity.[11]
  • EPEX - This hardware that was built into the SFU was meant to do experiments related to fuel creation and management in space.[12]
  • MEX - This software was meant to review and research the effects of various types of liquid within a space environment.[13]
  • BIO - This test involved observingJapanese fire belly newt eggs hatch in deep space.[14]

See also

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References

[edit]
  1. ^McDowell, Jonathan."Satellite Catalog".Jonathan's Space Page. Retrieved29 October 2013.
  2. ^abc- Main Reference-Main Reference
  3. ^Chronology DataArchived 2006-09-28 at theWayback Machine-Chronology Data
  4. ^"SFU : Space Flyer Unit". Archived fromthe original on 2016-08-01. Retrieved2016-08-01.
  5. ^PurposesArchived 2006-09-28 at theWayback Machine-Purposes
  6. ^abExperiment Data 1Archived 2006-09-28 at theWayback Machine-Experiment Data 1
  7. ^Experiment Data 2Archived 2006-09-28 at theWayback Machine-Experiment Data 2
  8. ^Irts DataArchived 2005-11-27 at theWayback Machine-IRTS Data
  9. ^2d array data-2d Array Data
  10. ^hvsa dataArchived 2005-11-25 at theWayback Machine-hvsa data
  11. ^Sdpd dataArchived 2005-11-25 at theWayback Machine-Sdpd data
  12. ^epex dataArchived 2005-11-25 at theWayback Machine-epex data
  13. ^mexArchived 2005-11-25 at theWayback Machine-mex data
  14. ^bioArchived 2005-11-25 at theWayback Machine-Bio

Further reading

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External links

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