Mars Pathfinder heatshield design and flight experience

Authors
Citation
Wh. Willcockson, Mars Pathfinder heatshield design and flight experience, J SPAC ROCK, 36(3), 1999, pp. 374-379
Citations number
14
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF SPACECRAFT AND ROCKETS
ISSN journal
00224650 → ACNP
Volume
36
Issue
3
Year of publication
1999
Pages
374 - 379
Database
ISI
SICI code
0022-4650(199905/06)36:3<374:MPHDAF>2.0.ZU;2-4
Abstract
The Mars Pathfinder lander mission represented the first return to the surf ace of Mars In over 20 years, Along with the Mars Global Surveyor orbiter, it represented a new era in faster, cheaper, better planetary missions, dra matically reducing costs below previous Mars programs. The design experienc e of the entry aeroshell, which protected the lander during its hypersonic entry into the Martian atmosphere, is described. The design of the aeroshel l required a cooperative effort between Martin Marietta Corporation (now Lo ckheed Martin), the prime contractor, and multiple NASA field centers.