Human Spaceflights

International Flight No. 150

STS-46

Atlantis (12)

USA

hi res version (588 KB)

 

Launch, orbit and landing data

Launch date:  31.07.1992
Launch time:  13:56 UTC
Launch site:  Cape Canaveral (KSC)
Launch pad:  39-B
Altitude:  426 km
Inclination:  28,45°
Landing date:  08.08.1992
Landing time:  13:11 UTC
Landing site:  Cape Canaveral (KSC)

walkout photo

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alternate crew photo

alternate crew photo

alternate crew photo

Crew

No.   Surname Given names Position Flight No. Duration Orbits
1  Shriver  Loren James  CDR 3 7d 23h 15m  127 
2  Allen  Andrew Michael "Andy"  PLT 1 7d 23h 15m  127 
3  Nicollier  Claude  MSP 1 7d 23h 15m  127 
4  Ivins  Marsha Sue  MSP 2 7d 23h 15m  127 
5  Hoffman  Jeffrey Alan  MSP 3 7d 23h 15m  127 
6  Chang-Diaz  Franklin Ramon  MSP 3 7d 23h 15m  127 
7  Malerba  Franco Egidio  PSP 1 7d 23h 15m  127 

Crew seating arrangement

Launch
1  Shriver
2  Allen
3  Nicollier
4  Ivins
5  Hoffman
6  Chang-Diaz
7  Malerba
Landing
1  Shriver
2  Allen
3  Hoffman
4  Ivins
5  Nicollier
6  Chang-Diaz
7  Malerba

Backup Crew

No.   Surname Given names Position
7  Guidoni  Umberto  PSP

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Flight

Launch from Cape Canaveral (KSC); landing on Cape Canaveral (KSC).

Mission's primary objectives were the deployment of ESAs EURECA (European Retrievable Carrier) with 70 experiments onboard and the joint NASA/Italian Space Agency Tethered Satellite System (TSS). EURECA was deployed a day later than scheduled because of a problem with its data handling system. Seven and a half hours after deployment, the spacecraft's thrusters were fired to boost EURECA to its planned operating altitude of around 310 miles. However, thruster firing was cut to six minutes from 24 minutes by Mission Control in Darmstadt because of unexpected attitude data from the spacecraft. The problem was resolved and EURECA was successfully boosted to its operational orbit on the mission's sixth day. A year later EURECA was retrieved by the STS-57 mission.

The TSS deployment also was delayed one day because of the problems with EURECA. During deployment, the satellite reached a maximum distance of only 860 feet from the orbiter instead of the planned 12.5 miles because of a jammed tether line. After numerous attempts over several days to free the tether, TSS operations were curtailed and the satellite was stowed for return to Earth.

Secondary payloads included: Evaluation of Oxygen Integration with Materials/Thermal Management Processes (EOIM-III/TEMP 2A), Consortium for Materials Development in Space Complex Autonomous Payload (CONCAP II and CONCAP III), IMAX Cargo Bay Camera (ICBC), Limited Duration Space Environment Candidate Materials Exposure (LDCE), Air Force Maui Optical Site (AMOS), Pituitary Growth Hormone Cell Function (PHCF), and Ultraviolet Plume Instrument (UVPI). Mission extended extra day to complete scientific objectives.

Photos / Drawings


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Last update on July 25, 2012.