PAM-D with the Phoenix spacecraft. The stage is successively spun, fired, yo-yo de-spun and jettisoned.
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[]
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[]
References[]
- ↑ "Payload Assist Module (PAM)". Global Security. http://www.globalsecurity.org/space/systems/pam.htm. Retrieved June 8, 2012.
- ↑ 2.0 2.1 Template:Cite journal
External links[]
| File:Commons-Logo.svg | Wikimedia Commons has media related to Category:Payload Assist Module. |
- Payload Assist Module at the NASA Shuttle Reference Manual
- Payload Assist Module at GlobalSecurity.org
Template:Upper stages
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