STS-96
This is a mission of the United States Space Shuttle
| Space Shuttle program |
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| Mission Insignia |
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| Mission Statistics |
| Mission: | STS-96 |
| Shuttle: | Discovery |
| Launch Pad: | 39-B |
| Launch: | May 27, 1999 6:49a.m. EDT |
| Landing: | June 6, 1999 KSC's SLF 2:02:43 a.m. EDT (Runway 15) |
| Duration: | 9 days, 19 hours, 13 minutes, 57 seconds. |
| Orbit Altitude: | 173 nm |
| Orbit Inclination: | 51.6 degrees |
| Distance Traveled: | 6 million km |
| Crew photo |
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Previous Mission:
STS-88 |
Next Mission:
STS-93 |
Crew
Mission Parameters
Docking with ISS
- Docked: May 29, 1999, 04:23:55 UTC
- Undocked: June 3, 1999, 22:39:00 UTC
- Time Docked: 5 days, 18 h, 15 min, 5 s
Space walk
- Jernigan and Barry - EVA 1
- EVA 1 Start: May 30, 1999 - 02:56 UTC
- EVA 1 End: May 30, - 10:51 UTC
- Duration: 7 hours, 55 minutes
Mission Highlights
STS-96 is a logistics and resupply mission for the International Space Station. It will be the first flight to dock to the International Space Station. The SPACEHAB double module will carry internal and resupply cargo for station outfitting.
The Integrated Cargo Carrier (ICC) will carry the Russian cargo crane, known as STRELA, which will be mounted to the exterior of the Russian station segment, the SPACEHAB Oceaneering Space System Box (SHOSS) and a U.S. built crane called the ORU Transfer Device (OTD).
Other payloads on STS-96 are the Student Tracked Atmospheric Research Satellite for Heuristic International Networking Equipment (STARSHINE), the Shuttle Vibration Forces Experiment (SVF) and the Orbiter Integrated Vehicle Health Monitoring - HEDS Technology Demonstration (IVHM HTD).
The STARSHINE satellite consists of an inert, 19 inch (483 mm) hollow sphere covered by 1,000 evenly-distributed, flat, polished mirrors, each 1 inch in diameter. The payload consists of the STARSHINE satellite, integrated with the Pallet Ejection System (PES), then mounted inside a lidless carrier. The HH equipment consists of one HH Lightweight Avionics Plate (LAP), then mounted inside a lidless carrier. Additional HH equipment consists of one Hitchhiker Ejection System Electronics (HESE), one 5.0 cubic-foot (142 L) HH canister, and one Adapter Beam Assembly (ABA). The purpose of the mission is to train international student volunteer observers to visually track this optically reflective spacecraft during morning and evening twilight intervals for several months, calculate its orbit from shared observations, and derive atmospheric density from drag-induced changes in its orbit over time.
The Shuttle Vibration Forces (SVF) Experiment will provide flight measurements of the vibratory forces acting between an aerospace payload and its mounting structure. The force transducers will be incorporated into four custom brackets which will replace the existing brackets used to attach the 5 ft (1.5 m) standard canister to the side wall GAS adapter beam. The payload will be activated automatically by the Orbiter Lift-off vibration and will operate for approximately 100 seconds. STS-96 will be the second flight of the SVF experiment
The purpose of the Orbiter Integrated Vehicle Health Monitoring- HEDS Technology Demonstration (IVHM HTD) is to demonstrate competing modern, off-the-shelf sensing technologies in an operational environment to make informed design decisions for the eventual Orbiter upgrade IVHM. The objective of IVHM is to reduce planned ground processing, streamline problem troubleshooting (unplanned ground processing), enhance visibility into systems operation and improve overall vehicle safety.
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