Official name SFU
Alternative name SFU
Cospar ID 1995-011A
Norad ID 23521
Launch date 1995-03-18
Launch site TNSTA
Launch vehicle H-2 + SSB
Country/Organization Japan
Type application Microgravity, Astronomy (Infra red), Shuttle retrievable carrier
Operator NASDA
RCS size LARGE
Decay date 1996-01-20
Shape Cyl
Mass (kg) 3766.11
Diameter (m) 4.46
Height (m) 3.07
Span (m^2) 4.46
Contractors Mitsubishi Electric (MELCO)
Equipment IRTS
Power 2 deployable fixed solar arrays, batteries

SFU (Space Flyer Unit) was a Japanese space laboratory launched by the same H-2 + SSB rocket that launched GMS 5. It carried an infrared telescope (IRTS), and instruments and supplies for microgravity experiments.

IRTS was Japan's first orbiting telescope dedicated to infrared observations (1 - 1000 micron range) of the interstellar medium, late type stars and interplanetary dust. IRTS instrumentation was attached to a multi-purpose Space Flyer Unit (SFU). The four primary science instruments were the Near Infrared Spectrometer (NIRS), the Mid Infrared Spectrometer (MIRS), the Far-Infrared Line Mapper (FILM), and the Far-Infrared Photometer (FIRP). All instruments were located at the focal plane of a 15-cm aperture telescope. Approximately 7 percent of the sky was surveyed during a four-week period.

SFU was retrieved by the Shuttle STS 72 on 13 January 1996 after jettisoning the solar panels.

Satellite COSPAR Date LS Launch Vehicle Remarks
SFU 1995-011A 1995-03-18 TNSTA H-2 + SSB with GMS 5