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Other Designations: Shuttle Pallet Satellite). Class: Military. Type: SDI. Destination: Maximum Payload Orbit. Nation: USA. Agency: MBB. Manufacturer: MBB. The SPAS (Shuttle Pallet Satellite) satellite was a reusable free-flying vehicle built by Messerschmitt-Bolkow-Blohm, which could be deployed and then retrieved by the US Space Shuttle's Remote Manipulator System arm. The original SPAS, with materials processing and SDI-related sensor payloads, was used on several missions (STS-7, STS-11, STS-39). An experiment-carrying truss (USS) based on the original SPAS structure (but without the avionics and attitude control) was flown on the Spacelab D-1 and D-2 missions.
ORFEUS-SPAS, the Orbiting and Retrievable Far and Extreme UV Spectrometer, was a German astronomical satellite. It was be deployed by the shuttle remote manipulating system arm and retrieved after six days of free flight. The main instrument was a 1 meter telescope with extreme ultraviolet (400-1150 Angstroms) and far ultraviolet (900-1250 Angstrom) spectrometers of high spectral resolution. Also carried was the Princeton Interstellar Medium Absorption Profile Spectrograph which studied the fine structure of ultraviolet absorption lines in stellar spectra caused by interstellar gas. The ORFEUS program was managed by the German space agency.
CRISTA-SPAS, equipped for observation of the earth's atmosphere, was flown on two missions. Typical orbit: 295 km x 300 km at 29 degrees inclination. Mass: 3,230 kg (7,120 lb). Associated Launch Vehicle: Shuttle. SPAS Chronology
- 1984 February 3 - SPAS 1A - Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.
German-built Shuttle Pallet Satellite (SPAS), first flown on STS-7, became first satellite refurbished and flown again. SPAS remained in payload bay due to electrical problem with Remote Manipulator System (RMS).
- 1993 September 12 - ORFEUS-SPAS - Launch Site: Cape Canaveral. Launch Vehicle: Shuttle. Mass: 3,202 kg (7,059 lb). Perigee: 301 km (187 mi). Apogee: 331 km (205 mi). Inclination: 28.50 deg. Period: 90.90 min.
Deployed from STS-51.
- 1997 August 7 - CRISTA - Launch Site: Cape Canaveral. Launch Vehicle: Shuttle. Perigee: 282 km (175 mi). Apogee: 296 km (183 mi). Inclination: 57.00 deg. Period: 90.30 min.
Recaptured August 16.
Bibliography and Further Reading
- NASA GSFC Orbital Parameters, .
- McDowell, Jonathan, Jonathan's Space Report (Internet Newsletter), Harvard University, Weekly, 1989 to Present. Essential internet newsletter recording worldwide weekly space events. Accessed at: http://www.planet4589.org/jsr.html.
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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