STS-85

USA


Manned Flight n°: 201

Earth orbit Flight n°: 198

USA manned Flight n°: 117


Launch, orbit & landing data:

Designation 24889 / 97039A
Launch date - time 07 Aug 1997 - 14:41:00 UT
Launch site KSC, LC39A
Launch vehicle  Space Shuttle
Orbiter Discovery #23 (OV-103)
Primary payload CRISTA-SPAS
Mass (kg) 
Earth orbit on :
   - Perigee / Apogee 320 km
   - Inclination 51.6°
   - Period  min
Landing date - time 19 Aug 1997 - 11:07:59 UT
Landing location KSC, Runway 33
Flight Duration (d:hr:min) 11d 20h 28m
Nbr orbits 189

Flight Crew

Nr. Surname Given name Job Duration
1  Brown  Curtis Lee, Jr.  CDR 11d 20h 28m 
2  Rominger  Kent Vernon  PLT 11d 20h 28m 
3  Davis  Nancy Jan  MSP 11d 20h 28m 
4  Curbeam  Robert Lee, Jr.  MSP 11d 20h 28m 
5  Robinson  Stephen Kern  MSP 11d 20h 28m 
6  Tryggvason  Bjarni Valdimar  PSP 11d 20h 28m 

Mission details:

Launch from Cape Canaveral (KSC); landing on Cape Canaveral (KSC); deploying and retrieval of German-built satellite CRISTA-SPAS-02; several scientific experiments; tests with Utraviolet Spectrograph Telescope and Camera; testing tools for ISS (e.g. Japanese-built robot-arm).

07 August 1997 14:41 GMT. Duration: 11.85 days. Agency: NASA Payload: Discovery F23 / CRISTA-SPAS-2. Perigee: 249 km. Apogee: 261 km. Inclination: 57.0 deg. Period: 89.6 min.

Deployed and retrieved the CRISTA-SPAS-2 (the Cryogenic Infrared Spectrometers and Telescopes for the Atmosphere-Shuttle Pallet Satellite-2) designed to study Earth's middle atmosphere. The CRISTA-SPAS-2 was making its second flight on the Space Shuttle and represented the fourth mission in a cooperative venture between the German Space Agency (DARA) and NASA.

CRISTA-SPAS was deployed by the RMS arm at 22:27 GMT on August 7 and was recaptured by Discovery's RMS arm at 15:14 GMT on August 16. Because of unfavorable weather conditions at the primary shuttle landing site at the Kennedy Space Center, Discovery was waved off for its scheduled August 18 landing. STS-85 landed the next day, at Kennedy Space Center at 11:08 GMT.

Cargo Bay Payloads:

  • Bay 1-2: External Airlock
  • Bay 5: MPESS (Multi Purpose Experiment Support Structure) with the MFD (Manipulator Flight Demonstration) payload from the Japanese space agency. This was a 'robot hand' that will be at the end of the robot arm being developed for the Japanese space station module.
  • Bay 6 Port sidewall: A small carrier with the ITEPC radiation dose counter.
  • Bay 7: MPESS with the TAS-01 payload (Technology Applications and Science) from NASA-Goddard's Hitchhiker-M program. TAS-01 consisted of several GAS cans with science experiments, including the second flight of the Shuttle Laser Altimeter and an instrument to measure the absolute bolometric flux of the Sun.
  • Bay 9: ASTRO-SPAS, a free flying platform built by Germany's DASA, carrying the CRISTA-SPAS atmospheric science payload on its second mission.
  • Bay 11 Port sidewall: a small carrier with the ERPCL transmitter/receiver which communicates with SPAS during its flight.
  • Bay 12: MPESS with the IEH-2 Hitchhiker payload from Goddard. The International Extreme Ultraviolet Hitchhiker was a joint NASA-Italian astronomy payload. Its two main instruments were the UVSTAR ultraviolet spectrograph and the SEH solar extreme ultraviolet instrument. The MPESS also carried the GLO-5 and GLO-6 airglow studies and the Data-Chaser technology experiment. UVSTAR's main objective is to study the extreme UV emissions from the Io plasma torus around Jupiter.
  • Bay 13 Starboard sidewall: GABA (GAS Beam Adapter) with two GAS experiment cans, G-572 and G-745. G-572 has experiments from Bellermine College and Utah State, and G-745 has student experiments from Mayo High School.
  • In-Cabin Payloads: BDS-03; BRIC; PCG-STES-05; ACIS; MSX; SIMPLEX; SWUIS; SSCE.

    Developmental Test Objectives
    Detailed Supplementary Objectives
    Risk Mitigation Experiments

  • DTO 255: Wraparound DAP Flight Test Verification
  • DTO 312: External Tank TPS Performance
  • DTO 700-10: Orbiter Space Vision System Videotaping
  • DTO 700-12: Global Positioning System/Inertial Navigation System
  • DTO 700-14: Single String Global Positioning System
  • DTO 805: Crosswind Landing Performance
  • DTO 842: AutoTRAC Computer Vision System
  • DTO 843: V-Bar Proximity Operations Demonstration for ISS
  • DTO 844: RMS Situational Awareness Displays
  • DSO 331: Integration of the Space Shuttle Launch and Entry Suit
  • DSO 484C: Assessment of Sleep Quality and Circadian Rhythms in Astronauts
  • DSO 485: Intermars Tissue Equivalent Proportional Counter
  • DSO 493: Monitoring Latent Virus Reaction and Shedding in Astronauts
  • DSO 802: Educational Activities
  • RME 1328: Microgravity Vibration Isolation Mount System Performance

    Payload And Vehicle Masses: Orbiter (Discovery) empty and 3 SSME's: 69,775 kg; Shuttle System at SRB Ignition 2,047,303 kg; Orbiter Weight at Landing with Cargo 98,847 kg; CRISTA-SPAS 3503 kg; IEH-02 1460 kg; MFD 1647 kg; TAS-01 2516 kg; SWUIS 62 kg.


    Ref.: #7, #8, #16 - update: 25.03.06 Home