STS-87 was a Space Shuttle mission launched from Launch Complex 39B of the Kennedy Space Center on 19 November 1997. It was the 88th flight of the Space Shuttle and the 24th flight of Columbia.

1997年11月19日 · The STS-87 mission launched aboard the Space Shuttle Columbia on November 19, 1997. The primary payload for the mission was the U.S. Microgravity Payload-4 (USMP-4).

STS-87 是历史上第87次航天飞机任务，也是 哥倫比亞號太空梭 的第21次太空飞行。

1997年11月19日 · STS-87 carried out the mission USMP-4 (United States Microgravity Payload). The United States Microgravity Payload (USMP-4) is a Spacelab project managed by Marshall Space Flight Center, Huntsville, Alabama. The complement of microgravity research experiments is divided between two Mission-Peculiar Experiment Support Structures (MPESS) in the ...

sts-87 是歷史上第87次穿梭機任務，也是哥倫比亞號穿梭機的第21次太空飛行。

Experiments aboard the USMP-4 laboratory centered around materials science, combustion science and fundamental physics. Specific investigations included the Advanced Automated Directional Solidification Furnace (AADSF), Confined Helium Experiment (CHeX) and Isothermal Dendritic Growth Experiment (IDGE).

Loss of external tank intertank foam results in over 100 hits on orbiter heat shield. AKA: Columbia. Launched: 1997-11-19. Returned: 1997-12-05. Number crew: 6 . Duration: 15.69 days. Spartan 201 was released a day late on November 21.

2024年4月8日 · This was the fourth flight of the U.S. Microgravity Payload. Another payload was deployed, but to maneuver properly. It was retrieved, but not without difficulty. A lengthy EVA was performed to capture the satellite manually. Crew. Archived NASA mission page for STS-87. Page last modified: 08 April 2024 17:42:35.

summarizes the activities of the STS-87 mission and presents a summary of the External Tank (ET), Solid Rocket Booster (SRB), Reusable Solid Rocket Motor (RSRM), and Space Shuttle main engine (SSME) performance during this eighty-eighth mission of the Space Shuttle Program. STS-87 was the sixty-second flight since the return to

STS-87 (USMP-4) results. Section 1 briefly outlines the OARE system features, coordinates, and measurement parameters. Section 2 describes the results from STS-87. The mission description, data calibration, and representative data obtained on STS-87 are presented. Finally, Section 3 presents a discussion of accuracy achieved and achievable with ...