Other payloads included Continuous Flow Electrophoresis System (CFES) III, Radiation Monitoring Equipment (RME), one SSIP experiment, IMAX camera system and the U.S. It demonstrated that large, lightweight solar arrays were feasible for future use in space station applications.
#Orbiter processing facility full#
The wing carried different types of solar cells and was extended to its full height several times. The 102-foot-tall, 13-foot-wide Office of Application and Space Technology-1 (OAST-1) solar wing was unfolded from the payload bay. The Kennedy’s orbiter processing facility has its own unique set of challenges to overcome.
Kennedy’s orbiter prepared the missions for both military and civilians. Three satellites were deployed, including the Satellite Business Systems SBS-D, SYNCOM IV-2 (also called LEASAT-2) and TELSTAR. The Kennedy’s orbiter processing facility is one of the most critical links in the shuttle chain. Landing was held at the desert runway as opposed to the concrete runway at Edwards because this was Discovery’s maiden flight. Mission duration was 6 days, 0 hours, 56 minutes, 4 seconds. PDT at Runway 17, Edwards Air Force Base, California. August 30 launch was delayed 6 minutes, 50 seconds when a private aircraft intruded into a “no-fly” warning area off the coast of Cape Canaveral.
#Orbiter processing facility software#
To preserve the launch schedule of future missions, the STS-41D cargo was remanifested to include elements of STS-41F, which was canceled.Ī third launch attempt on Augwas delayed when a discrepancy was noted in flight software of Discovery’s Master Events Controller (MEC). Discovery was returned to the Orbiter Processing Facility where the engine was replaced. Main engines were shut down at T-4 seconds when GPC detected an anomaly in Main Engine Number Three. Launch attempt on Jended in the first main engine cutoff of the Shuttle program. Launch attempt on Jwas scrubbed during the T-9 minute hold due to failure of the Shuttle’s back-up General Purpose Computer (GPC). Rollover to Vehicle Assembly Building – August 1, 1984 Rollover to Orbiter Processing Facility – July 17, 1984 Rollback to Vehicle Assembly Building – July 14, 1984 Rollover to Vehicle Assembly Building – May 12, 1984 Rollover to Orbiter Processing Facility – January 10, 1984 Rollover to Vehicle Assembly Building (for storage) – December 9, 1983 Tow to Orbiter Processing Facility – November 10, 1983
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