Human Spaceflights

International Flight No. 184

STS-75

Columbia (19)

USA

hi res version (622 KB)

Source: www.spacepatches.nl

Launch, orbit and landing data

Launch date:  22.02.1996
Launch time:  20:18 UTC
Launch site:  Cape Canaveral (KSC)
Launch pad:  39-B
Altitude:  296 km
Inclination:  28,45°
Landing date:  09.03.1996
Landing time:  13:58 UTC
Landing site:  Cape Canaveral (KSC)

walkout photo

hi res version (1,03 MB)

alternate crew photo

Crew

No.   Surname Given names Position Flight No. Duration Orbits
1  Allen  Andrew Michael "Andy"  CDR 3 15d 17h 41m  251 
2  Horowitz  Scott Jay "Doc"  PLT 1 15d 17h 41m  251 
3  Hoffman  Jeffrey Alan  MSP 5 15d 17h 41m  251 
4  Cheli  Maurizio  MSP 1 15d 17h 41m  251 
5  Nicollier  Claude  MSP 3 15d 17h 41m  251 
6  Chang-Diaz  Franklin Ramon  MSP 5 15d 17h 41m  251 
7  Guidoni  Umberto  MSP 1 15d 17h 41m  251 

Crew seating arrangement

Launch
1  Allen
2  Horowitz
3  Hoffman
4  Cheli
5  Nicollier
6  Chang-Diaz
7  Guidoni
Landing
1  Allen
2  Horowitz
3  Nicollier
4  Cheli
5  Hoffman
6  Chang-Diaz
7  Guidoni

Flight

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

The mission "US Microgravity Payload-3" carried several experiment in different sientific fields. The USMP-3 payload consisted of four major experiments mounted on two Mission Peculiar Experiment Support Structures (MPESS) and three Shuttle Mid-deck experiments. The experiments were: Advanced Automated Directional Solidification Furnace (AADSF), Material pour l'Etude des Phenomenes Interessant la Solidification sur Terre et en Orbite (MEPHISTO), Space Acceleration Measurement System (SAMS), Orbital Acceleration Research Experiment (OARE), Critical Fluid Light Scattering Experiment (ZENO) and Isothermal Dendritic Growth Experiment (IDGE).

But the primary objective of STS-75 was to carry the Tethered Satellite System Reflight (TSS-1R) into orbit and to deploy it spaceward on a conducting tether. The deploying of the Italian Tethered Satellite System-1 failed, because the tether has broken after a distance of 19 km. The satellite was lost. The specific TSS-1R mission objectives were: characterize the current-voltage response of the TSS orbiter system, characterize the satellite's high-voltage sheath structure and current collection process, demonstrate electric power generation, verify tether control laws and basic tether dynamics, demonstrate the effect of neutral gas on the plasma sheath and current collection, characterize the TSS radio frequency and plasma wave emissions and characterize the TSS dynamic-electrodynamic coupling. TSS-1R Science Investigations included: TSS Deployer Core Equipment and Satellite Core Equipment (DCORE/SCORE), Research on Orbital Plasma Electrodynamics (ROPE), Research on Electrodynamic Tether Effects (RETE), Magnetic Field Experiment for TSS Missions (TEMAG), Shuttle Electrodynamic Tether System (SETS), Shuttle Potential and Return Electron Experiment (SPREE), Tether Optical Phenomena Experiment (TOP), Investigation of Electromagnetic Emissions by the Electrodynamic Tether (EMET), Observations at the Earth's Surface of Electromagnetic Emissions by TSS (OESSE), Investigation and Measurement of Dynamic Noise in the TSS (IMDN), Theoretical and Experimental Investigation of TSS Dynamics (TEID) and the Theory and Modeling in Support of Tethered Satellite Applications (TMST).

STS-75 also was the first use of an operating system based on Linux kernel on orbit. An older Digital Unix program, originally on DEC Alpha servers, was ported to run on Linux on a laptop. The next use of Linux was a year later, on STS-83.

The mission was extended one day due of bad weather at Cape Canaveral (KSC).

Photos / Drawings

 

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Last update on July 28, 2012.