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Table 3-1
SRMS FLIGHTS

[[5 Columned Table]]
|FLIGHT|LAUNCH DATE|SRMS SERIAL NUMBER*|PAYLOAD/MASS (KG)|REMARKS
|---|---|---|---|---|
|STS-2|4 Nov 81|201|Unloaded|Unloaded arm tests. Thermal performance.|
|STS-3|22 Mar 82|201|Plasma Diagnostics Package (PDP) 156 kg|Unloaded and lightly loaded arm tests. Thermal performance.|
|STS-4|27 June 82|201|Induced Environment Contamination Monitor (IECM) 370 kg|Unloaded and lightly loaded arm tests. Thermal performance.|
|STS-7|18 June 83|201|Shuttle Pallet Satellite (SPAS-01) 1439 kg|Payload retrieval and release. Tip-off rate.|
|STS-8|30 Aug 83|201|Payload Flight Test Article (PFTA) 3384 kg|Medium loaded arm tests.|
|41-B|3 Feb 84|201|SPAS-01 Manned Foot Restraint (MFR) with EVA Astronaut|Manoeuvering Astronaut on MFR.|
|41-C|6 Apr 84|302|Long Duration Exposure Facility (LDEF) 8768 kg Solar Maximum Mission (SMM) MFR with EVA Astronaut|Deployment and release of LDEF. Retrieval of Rotating Solar Max. Work platform for EVA Astronauts.|
|41-D|30 Aug 84|301|Solar Array Experiment (SAE)|SRMS used to "knock" ice off the Orbiter.|
|41-G|8 Oct 84|302|Earth Radiation Budget Satellite (ERBS)|Deployment and release of ERBS. SRMS used to latch shuttle antennas.|
|51-A|6 Nov 84|301|Palapa, Westar, Manned Manoeuvering Unit (MMU), MFR, Astronaut|SRMS used to manoeuvre astronaut/MFR and astronaut MMU/Palapa combination.|

*201 is the SRMS development test model; 301 and 302 are operational flight models of the SRMS.

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