Langley view of the Shuttle Erectable Antenna
AKA: Atlantis. Launched: 1985-11-27. Returned: 1985-12-03. Number crew: 7 . Duration: 6.88 days. Location: First Mexican astronaut..
Payloads: Deploy SATCOM (RCA-Satellite Communications) Ku-2 with Payload Assist Module (PAM)-D II. Deploy Morelos (Mexico communications satellite)-B with PAM-D. Deploy AUSSAT (Australian communications satellite)-2 with PAM-D. EASE/ACCESS (Assembly of Structures— Assembly Concept for Construction of Erectable Space Structures) by extravehicular activity (EVA) astronauts, Continuous Flow Electrophoresis System (CFES), Diffusive Mixing of Organic Solutions (DMOS), IMAX camera, one getaway special (GAS), Linhof camera and Hasselblad camera.
Orbits of Earth: 108. Distance traveled: 4,568,882 km. Orbiter Liftoff Mass: 118,664 kg. Orbiter Mass at Landing: 93,316 kg. Payload to Orbit: 21,791 kg. Payload Returned: 9,282 kg. Landed at: Concrete runway 22 at Edwards Air Force Base, Cali. Landing Speed: 350 kph. Touchdown miss distance: 727 m. Landing Rollout: 3,279 m. EVA: Jerry Ross and Sherwood Spring, EVA No. 1, duration 5 hours, 34 minutes. EVA No. 2, duration 6 hours, 46 minutes.
NASA Official Mission Narrative
Mission Name: 61-B (23)
Pad 39-A (35)
23rd Shuttle mission
2nd Flight OV-104
2nd Night launch
Brewster H. Shaw, Jr. (2), Commander
Bryan D. O'Connor (1), Pilot
Mary L. Cleave (1), Mission Specialist 1
Sherwood C. Spring (1), Mission Specialist 2
Jerry L. Ross (1), Mission Specialist 3
Rodolfo Neri Vela (1), Payload Specialist 1
Charles D. Walker (3), Payload Specialist 2
OPF - Oct. 12, 1985
VAB - Nov. 7, 1985
PAD - Nov. 12, 1985
November 26, 1985, 7:29:00 p.m. EST. Launch proceeded as scheduled with no delays. Launch Weight: 261,455 lbs.
Inclination: 28.5 degrees
Duration: Six days, 21 hours, four minutes, 49 seconds.
Distance: 2,838,972 miles
ET : 22/LWT-15
MLP : 2
December 3, 1985, 1:33:49 p.m. PST, Runway 22, Edwards Air Force Base, Calif. Rollout distance: 10,759 feet. Rollout time: 78 seconds. Mission shortened one revolution due to lightning conditions at Edwards. Landed on concrete runway because lake bed was wet. Orbiter returned to KSC Dec. 7, 1985. Landing Weight: 205,732 lbs.
Three communications satellites deployed: MORE LOS-B (Mexico), AUSSAT-2 (Australia) and SATCOM KU-2 (RCA Americom). MORELOS-B and AUSSAT-2 attached to Payload Assist Module-D motors, SATCOM KU-2 to a PAM-D2 designed for heavier payloads. Two experiments conducted to test assembling erectable structures in space: Experimental Assembly of Structures in Extravehicular Activity (EASE) and Assembly Concept for Construction of Erectable Space Structure (ACCESS). Experiments required two space walks by Spring and Ross lasting five hours, 32 minutes, and six hours, 38 minutes, respectively. Middeck payloads: Continuous Flow Electrophoresis System (CFES); Diffusive Mixing of Organic Solutions (DMOS); Morelos Payload Specialist Experiments (MPSE) and Orbiter Experiments (OEX). In payload bay: Get Away Special and IMAX Cargo Bay Camera (ICBC).
Astronaut Jerry Ross at threshold of airlock compartment following EVA
Astronaut Jerry Ross on RMS holds on to ACCESS device
Astronaut Sherwood Spring on RMS checks joints on the ACCESS device
Astronauts Jerry Ross and Sherwood Spring assemble ACCESS components
Close-up view of the RCA Satcom K-2 communications satellite
Deployment of the RCA Satcom K-2 communications satellite
Manned seven crew. Deployed Morelos 2, Aussat 2, Satcom K2, OEX. Payloads: Deploy SATCOM (RCA-Satellite Communi-cations) Ku-2 with Payload Assist Module (PAM)-D II. Deploy Morelos (Mexico communications satellite)-B with PAM-D. Deploy AUSSAT (Australian communications satellite)-2 with PAM-D. EASE/ACCESS (Assembly of Structures— Assembly Concept for Construction of Erectable Space Structures) by extravehicular activity (EVA) astronauts, Continuous Flow Electrophore-sis System (CFES), Diffusive Mixing of Organic Solutions (DMOS), IMAX camera, one getaway special (GAS), Linhof camera and Hasseblad camera.