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Space Flyer Unit

Space Flyer Unit photographed from Endeavour during STS-72 mission
Mission type	Technology
Operator	NASDA ISAS NEDO USEF
COSPAR ID	1995-011A
SATCAT no.	23521
Website	www.isas.jaxa.jp/e/enterp/missions/sfu.shtml
Mission duration	10 months
Spacecraft properties
Manufacturer	Mitsubishi Electric
Launch mass	3,846 kilograms (8,479 lb)
Landing mass	3,492 kilograms (7,699 lb)
Start of mission
Launch date	18 March 1995, 08:01 (1995-03-18UTC08:01Z) UTC
Rocket	H-II 3F
Launch site	Tanegashima Yoshinobu 1
End of mission
Recovered by	Space Shuttle Endeavour STS-72
Recovery date	13 January 1996 (1996-01-14)
Landing date	20 January 1996, 07:41:41 UTC
Landing site	Kennedy SLF Runway 15
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Perigee altitude	470 kilometres (290 mi)
Apogee altitude	492 kilometres (306 mi)
Inclination	28.4 degrees
Period	94.22 minutes
Epoch	17 April 1995

The Space 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.

Technical data

The Space Flyer Unit was launched from Tanegashima Space Center from a H-II vehicle. It carried testing materials and research data that held value to NASA. The crew of STS-72 aboard Space Shuttle Endeavour retrieved the satellite on January 20, 1996, 10 months after it was launched. 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 Institute of Space and Astronautical Science, the National Space Development Agency, and Ministry of International Trade and Industry.

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

Purpose

The original purposes behind the SFU were to

• 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

A variety of systems that were operational within the SFU had never been implemented before. Equipment on board supported an infrared 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. The core system that was built into the SFU contained an octagonal aluminum truss. Inside of that were eight boxes of trapezoidal shape. The SFU was connected directly to the Kagoshima Space Center.

Experimentation data

There were a number of various types of experiments that were 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.
• 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.
• 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.
• 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.
• EPEX - This hardware that was built into the SFU was meant to do experiments related to fuel creation and management in space.
• MEX - This software was meant to review and research the effects of various types of liquid within a space environment.
• BIO - This test involved observing Japanese fire belly newt eggs hatch in deep space.

See also

• List of largest infrared telescopes

References

1. McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 29 October 2013.
2. ^ - Main Reference-Main Reference
3. Chronology Data Archived 2006-09-28 at the Wayback Machine-Chronology Data
4. "SFU : Space Flyer Unit". Archived from the original on 2016-08-01. Retrieved 2016-08-01.
5. Purposes Archived 2006-09-28 at the Wayback Machine-Purposes
6. ^ Experiment Data 1 Archived 2006-09-28 at the Wayback Machine-Experiment Data 1
7. Experiment Data 2 Archived 2006-09-28 at the Wayback Machine-Experiment Data 2
8. Irts Data Archived 2005-11-27 at the Wayback Machine-IRTS Data
9. 2d array data-2d Array Data
10. hvsa data Archived 2005-11-25 at the Wayback Machine-hvsa data
11. Sdpd data Archived 2005-11-25 at the Wayback Machine-Sdpd data
12. epex data Archived 2005-11-25 at the Wayback Machine-epex data
13. mex Archived 2005-11-25 at the Wayback Machine-mex data
14. bio Archived 2005-11-25 at the Wayback Machine-Bio

Further reading

• Kuriki, Kyoichi; Ninomiya, Keiken; Takei, Mitsuru; Matsuoka, Shinobu (2002), "Lessons learned from the space flyer unit (SFU) mission", Acta Astronautica, 51 (11): 797–806, Bibcode:2002AcAau..51..797K, doi:10.1016/S0094-5765(02)00026-7, PMID 12369586

External links

• ISAS Data
• Data Page

• Satellites of Japan
• Spacecraft launched in 1995
• Infrared telescopes
• Space hardware returned to Earth intact