STS-46

USA


Manned Flight n°: 153

Earth orbit Flight n°: 150

USA manned Flight n°: 80


Launch, orbit & landing data:

Designation 22064 / 92049A
Launch date - time 31 Jul 1992 - 13:56:48 UT
Launch site KSC, LC39B
Launch vehicle  Space Shuttle
Orbiter Atlantis OV-104 (#12)
Primary payload Eureca 1
Mass (kg) 
Flight Crew Shriver, Allen, Nicollier, Ivins
Hoffman, Chang-Diaz, Malerba
Call Sign 
Earth orbit on :
   - Perigee / Apogee  km
   - Inclination 28.45°
   - Period  min
Landing date - time 08 Aug 1992 - 13:11:51 UT
Landing location KSC, Runway 33
Flight Duration (d:hr:min) 7d 23h 15m
Nbr orbits 127

Crew

Nr. Surname Given name Job Duration
1  Shriver  Loren James  CDR 7d 23h 15m 
2  Allen  Andrew Michael  PLT 7d 23h 15m 
3  Hoffman  Jeffrey Alan  MSP 7d 23h 15m 
4  Chang-Diaz  Franklin Ramon  MSP 7d 23h 15m 
5  Nicollier  Claude  MSP 7d 23h 15m 
6  Ivins  Marsha Sue  MSP 7d 23h 15m 
7  Malerba  Franco Egidio  PSP 7d 23h 15m 

Mission details:

Launch from Cape Canaveral (KSC); landing on Cape Canaveral (KSC); deployment of ESA's European Retrievable Carrier (EURECA) was successfull after a few problems; deployment of joint NASA-Italian Space Agency Tethered Satellite System (TSS-1); maximum distance only 860 feet because of jammed tether line; TSS-operations were then stopped and the satellite was succesful stowed for return to Earth; several secondary payloads.

31 July 1992 13:57 GMT. Duration: 7.97 days.Agency: U.S. Air Force.Payload: Atlantis F12 / Eureca 1 / TSS 1. Mass: 12,965 kg. Perigee: 425 km. Apogee: 437 km. Inclination: 28.5 deg. Period: 93.2 min.

Manned seven crew. Deployed Eureca-1; failed to deploy Italian tether probe TSS-1. Payloads: Tethered Satellite System (TSS)-1; European Retrievable Carrier (EURECA)-1L; Evaluation of Oxygen Integration with Materials (EOlM)-lll/ Thermal Energy Management Processes (TEMP)-2A; Consortium for Materials Development In Space Complex Autonomous Payloads (CONCAP)-ll and Ill; IMAX Cargo Bay Camera (ICBC); Limited Duration Space Environment Candidate Materials Exposure (LDCE); Pituitary Growth Hormone Cell Function (PHCF); Ultravio-let Plume Instrument (UVPl).

Orbits of Earth: 127. Distance traveled: 5,344,642 km. Orbiter Liftoff Mass: 116,133 kg. Orbiter Mass at Landing: 94,711 kg. Payload to Orbit: 12,965 kg. Payload Returned: 8,434 kg. Landed at: Runway 33 at Kennedy Space Center, Florida. Landing Speed: 378 kph. Touchdown miss distance: 594 m. Landing Rollout: 3,310 m.



NASA Official Mission Narrative

Mission Name: STS-46 (49)
Atlantis (12)
Pad 39-B (20)
49th Shuttle Mission
12th Flight of OV-104
KSC Landing (11)

Crew:
Loren J. Shriver (3), Commander
Andrew M. Allen (1), Pilot
Jeffrey A. Hoffman (3), Mission Specialist 1
Franklin R. Chang-Diaz (3), Mission Specialist 2
Claude Nicollier (1), Mission Specialist 3
Marsha S. Ivins (2), Mission Specialist 4
Franco Malerba (1), Payload Specialist 1

Milestones:
OPF1 - 4/2/92
VAB - 6/4/92
PAD - 6/11/92

Payload:
TSS-1,EURECA-II,LDCE,PHCF,UVPI,IMAX-06,EOIM-III/TEMP-2A,CONCAP-II,ICBC,
AMOS
Mission Objectives:

Launch: July 31, 1992, 9:56:48 a.m. EDT. Launch Weight: 256,031 lbs.
Orbit:
Altitude: 230 nm
Inclination: 28.45 degrees
Orbits: 127
Duration: 7 days, 23 hours, 15 minutes, 3 seconds.
Distance: 3,321,007 miles

Hardware:
SRB: BI-052
SRM: 360W/L025
ET : 50/LWT-43
MLP : 1
SSME-1: SN-2032
SSME-2: SN-2033
SSME-3: SN-2027

Landing:
August 8, 1992, 9:11:50 a.m. EDT, Runway 33, Kennedy Space Center. Rollout distance: 10,860 feet. Mission extended one day to complete scientific objectives. Landing Weight: 208,806 lbs.

Mission Highlights:
Mission's primary objectives were the deployment of ESA's European Retrievable Carrier (EURECA) 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 31O miles. However, thruster firing was cut to six minutes from 24 minutes 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. TSS deployment also was delayed one day because of the problems with EURECA. During deployement, the satellite reached a maximum distance of only 86O 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. Seconday 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.


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