Research Payload Module 481 USAF heat pipe experiment. Technology satellite for Los Alamos National Laboratory (LANL), USA. Launched 1967. |
DoD 82-1 Cirris cryogenic infrared radiance instrument to obtain spectra of rocket and aircraft target exhausts. Lens cap failed to deploy. |
SPAS American military strategic defense satellite. |
SPAS 01 Retrievable satellite satellite built by MBB, Germany. Launched 1983. |
DFI Development Flight Instrumentation Pallet, included in shuttle bay on early missions. |
PFTA Shuttle Payload Flight Test Article, originally scheduled for launch on STS-16, but ultimately brought forward to STS-8 due to payload delays. It was an aluminum structure resembling two wheels with a six-meter long central axle, ballasted with lead to give it a total mass of 3,855 kg (8,499 lb), which could be lifted by the shuttle's Canadarm robot arm to give astronauts experience in using the system. It was stored in the midsection of the payload bay. |
LFC/ORS Larger Format Camera/ Orbital Refueling System payload carried in shuttle bay. |
Spartan American solar satellite. The Spartan series consists of low-cost, Shuttle-launched, short-duration, sounding-rocket-type payloads. The payloads were retrievable and reusable with a turnaround time of 6 to 9 months. Spartan operated as an autonomous sub-satellite, and the data was stored on an internal tape recorder. Pointing and stabilization were achieved by an attitude control system capable of three-axis stabilized pointing to any target within +/- 3 arc-minutes. Shuttle retrievable satellite operated by NASA Goddard, USA. Launched 1985. |
CRNE Null |
EASE/ACCESS Experimental Assembly of Structures in EVA and the Assembly Concept for Construction of Erectable Space Structures (EASE/ACCESS), a pair of space shuttle experiments on STS-61-B. The experiments studied how quickly astronauts would become proficient at assembling space structures during extravehicular activity, how quickly they would become fatigued, and to explore various construction and maintenance techniques. The EASE structure consisted of six 29-kg aluminum beams which were assembled into a 3.7 m tetrahedral truss structure. ACCESS consisted of 93 struts which were assembled into a triangular tower. |
MSL-2 The Material Science Laboratory was a carrier system designed to utilize the residual space of the Shuttle cargo bay. Based on the multi-purpose experiment support structure (MPESS) carrier, it offered a full complement of power, data, and thermal control services to payloads mounted on it. |
Spartan 203 (Spartan Halley, HCED) Null |
SFSS Spartan Flight Support Structure was an MPESS class cross-bay truss structure on which Spartan 204 was mounted. |
SL 3 MPESS Null |
SLA-1/GAS Null |
Spartan-Halley The main objective of this version of the Spartan spacecraft was to obtain UV spectra of the coma and tail of Comet Halley in January 1986 shortly before its perihelion. This spacecraft was lost when Space Shuttle Challenger exploded on launch. |
SRL Space Radar Lab, mounted in space shuttle payload bay. Carried JPL's SIR-C Shuttle Imaging Radar and the German/Italian X-SAR radar. |
STS ASTRO Shuttle payload bay fixture for attachment of instruments. |
SMRM-FSS Solar Maximum Mission (SMM) satellite repair payload carried on the STS-41-C shuttle mission. |
SSBUV Shuttle Solar Backscatter UltraViolet spectrometer, an instrument carried in the space shuttle payload bay. |
BBXRT Broad Band X-ray Telescope, a Goddard Space Flight Center experiment carried on STS-35 in the ASTRO package. |
STP-1 Space Test Payload-1; unclassified military payload carried on DoD flight STS-39. |
MPESS-ASEM Space shuttle bay Multi Purpose Experiment Support Structure and ASEM Node Carrier, providing stowage for EVA equipment. |
EOIM Effects of Oxygen Interactions with Materials experiment. |
Spartan 201 UV-Ray Astronomy (Shuttle retrievable) satellite operated by NASA Goddard, USA. Launched 1993 - 1998. |
USS Experiment-carrying truss carried in the space shuttle cargo bay. Based on the original SPAS structure (but without the avionics and attitude control) flown on the Spacelab D-1 and D-2 missions. |
SHOOT Superfluid Helium On-Orbit Transfer Flight Demonstration, an experiment carried on the space shuttle STS-57 mission in June 1993. The experiment transferred a superfluid between two dewars in a low gravity environment at different flow rates. |
ISA Interstage Adapter ISA (Interstage Adapter) satellite launched with Clementine placed in a highly eccentric Earth orbit. It carried a set of space environment experiments. |
OAST NASA Office of Aeronautics and Space Technology payload mounted in the shuttle bay, testing a variety of new technologies. |
LITE Lidar In-Space Technology Experiment, carried in shuttle payload bay. Measured the Earth's cloud cover and tracked particles in the atmosphere. |
MAPS Measurement of Air Pollution from Satellites instrument carried in shuttle bay; measured the distribution of carbon monoxide in the Earth's lower atmosphere (3 to 10 kilometers above the surface), from latitude 57 degrees North to latitude 57 degrees South. |
Spartan 204 UV X-Ray Astronomy (Shuttle retrievable) satellite operated by NASA Goddard, USAF STP (Space Test Program), USA. Launched 1995. |
WSF American materials science satellite. The Wake Shield Facility was released and later retrieved by the Shuttle in a single mission. It generated an ultra-hard vacuum in its wake for production of semiconductors and other experiments. Material research, retrievable satellite operated by NASA, USA. Launched 1994 - 1996. |
Spartan 206 (OAST Flyer) Null |
GBA GAS bridge, structure mounted in the shuttle pay to carry Getaway Special payload cannisters. |
Spartan 207 (IAE) Null |
TEAMS Time-of-flight/energy/angle mass spectrograph to study electrons and ions. Instrument mounted in shuttle bay. |
ORUC Version of the Spacelab Pallet that carries various technology and scientific instruments. |
FSS Flight Support Structure, used in the shuttle bay for berthing the Hubble Space Telescope. |
Second Axial Carrier Second Axial Carrier, specially designed shuttle pallet that flew on Hubble space telescope servicing flights. It carried cameras, instruments, and spare materials used in servicing Hubble. |
SLP Spacelab pallet, used for mounting of instruments in shuttle payload bay. Versions designated OSTA, OSS, ASTRO, ATLAS, ORU, and MPESS were adaptations for various purposes. |
IEH The shuttle's International Extreme Ultraviolet (EUV) Hitchhiker Payload investigated the solar EUV flux, and the EUV emissions of Jupiter and hot stellar objects. |
MFD Japanese Manipulator Flight Demonstration payload contained in the shuttle bay. Demonstrated the performance of a robot arm similar to that later used on the Japanese portion of the ISS. The robot arm was operated by crew members in the Aft Flight Deck of the Shuttle Orbiter using hand controllers. |
Technology Applications and Science Experiment Technology Applications and Science experiment, mounted in space shuttle bay, from NASA-Goddard's Hitchhiker-M program. TAS-01 used a number of GAS cans with science experiments, including the second flight of the Shuttle Laser Altimeter and an instrument to measure the absolute bolometric flux of the Sun. |
EDO Shuttle payload bay Extended Duration Orbiter pallet which provided 167 kg of additional liquid hydrogen and 1417 kg of liquid oxygen. These were utilized by the shuttle's fuel cells, providing electricity, oxygen, and water sufficient to extend shuttle mission duration to 21 days. |
USMP United States Microgravity Payload, a complement of experiments mounted on two connected Spacelab Multipurpose Experiment Support Structures (MPESSs) |
Alpha Magnetic Spectrometer Particle physics experiment, carried on STS-91, which used a cross-bay carrier containing a 3,000 kg magnet and scintillator detectors used in a search for antiprotons and antinuclei in cosmic rays. A later version of AMS was delivered to and installed on the International Space Station on STS-134. |
EAL/ODS External airlock / orbiter docking system, carried in the shuttle bay on missions requiring docking with the Mir space station. |
SpinSat SpinSat was a Naval Research Lab satellite to test new microthrusters for attitude control. The Japanese JEM-RMS robot arm extracted the SSIKLOPS (Cyclops) deployer and its attached SpinSat satellite from the Kibo airlock and positioned it for deployment. The Cyclops then ejected SpinSat into orbit. Technology, research (Atmospheric density), radio amateur communications satellite built by NRL for NRL, Space Test Program, USA. Launched 2014. |
Spartan 202 UV Astronomy (Shuttle retrievable) satellite operated by NASA Goddard, USA. |
Spartan 205 Plasma physics (Shuttle retrievable) satellite operated by NASA Goddard, USA. |
Spartan 208 (SSE) Null |
Spartan 211 Astronomy EUV (Shuttle retrievable) satellite built by, USA. |
WSF 4 Material research, retrievable satellite operated by NASA, USA. |
Ten experiments mounted on Shuttle Pallet Satellite (SPAS-01) performed research in forming metal alloys in microgravity and use of remote sensing scanner. Orbiter's small control rockets fired while SPAS-01 held by remote manipulator system to test movement on extended arm.
The Material Science Laboratory was a carrier system designed to utilize the residual space of the Shuttle cargo bay. Based on the multi-purpose experiment support structure (MPESS) carrier, it offered a full complement of power, data, and thermal control services to payloads mounted on it.
The Spartan series consists of low-cost, Shuttle-launched, short-duration, sounding-rocket-type payloads. The payloads were retrievable and reusable with a turnaround time of 6 to 9 months. Spartan operated as an autonomous sub-satellite, and the data was stored on an internal tape recorder. Pointing and stabilization were achieved by an attitude control system capable of three-axis stabilized pointing to any target within +/- 3 arc-minutes. The main objective of this spacecraft was to obtain UV spectra of the coma and tail of Comet Halley in January 1986 shortly before its perihelion. This spacecraft was lost when Space Shuttle Challenger exploded on launch.
Spartan Flight Support Structure was an MPESS class cross-bay truss structure on which Spartan 204 was mounted. The Spartan satellites were small free flyers deployed by the RMS robot arm for a couple of days and then retrieved. SPTN-204 carried NRL's FUVIS Far Ultraviolet Imaging Spectrograph which was used to study the Shuttle environment and make astronomical observations. This was the first Spartan mission to be sponsored by the USAF Space Test Program rather than NASA.
Technology Applications and Science experiment, mounted in space shuttle bay, from NASA-Goddard's Hitchhiker-M program. TAS-01 used a number of GAS cans with science experiments, including the second flight of the Shuttle Laser Altimeter and an instrument to measure the absolute bolometric flux of the Sun.
The Japanese JEM-RMS robot arm extracted the SSIKLOPS (Cyclops) deployer and its attached SpinSat satellite from the Kibo airlock and positioned it for deployment. The Cyclops then ejected SpinSat into orbit. SpinSat was a Naval Research Lab satellite to test new microthrusters for attitude control.