Payload Assist Module
The Payload Assist Module (PAM) is a modular upper stage designed and built by McDonnell Douglas (now Boeing), using Thiokol Star-series solid propellant rocket engines. The PAM was used with the Space Shuttle, Delta, and Titan launchers and carried satellites from low Earth orbit to a geostationary transfer orbit or an interplanetary course. The payload was spin stabilized by being mounted on a rotating plate.[1] Originally developed for the Space Shuttle, different versions of the PAM were developed:
- PAM-A (Atlas class), development terminated; originally to be used on both the Atlas and Space Shuttle
- PAM-D (Delta class), uses a Star-48B rocket motor
- PAM-DII (Delta class), uses a Star-63 rocket motor
- PAM-S (Special) as a kick motor for the space probe Ulysses
The PAM-D module, used as the third stage of the Delta II rocket, is the only version in use today.
2001 re-entry incident[edit]
On January 12, 2001, a PAM-D module re-entered the atmosphere after a "catastrophic orbital decay".[2] The PAM-D stage, which had been used to launch the GPS satellite 2A-11 in 1993, crashed in the sparsely populated Saudi Arabian desert, where it was positively identified.[2]
Gallery[edit]
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PAM-D stage in assembly
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SBS-3 satellite with PAM-D stage being launched from Space Shuttle Columbia
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Saudi officials inspect a PAM-D module that re-entered the atmosphere in 2001
References[edit]
- ^ "Payload Assist Module (PAM)". Global Security. Retrieved June 8, 2012.
- ^ a b "PAM-D Debris Falls in Saudi Arabia" (PDF). The Orbital Debris Quarterly News (NASA Johnson Space Center) 6 (2): 1. April 2001.
External links[edit]
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Wikimedia Commons has media related to Payload Assist Module. |
- Payload Assist Module at the NASA Shuttle Reference Manual
- Payload Assist Module at GlobalSecurity.org
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