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Thermal Engineering of Mars Entry Non-Ablative Aeroshell Part 1 Technical Alliance Group
- Format:
- Conference/Event
- Author/Creator:
- Wise, Robert A., author.
- Conference Name:
- International Conference On Environmental Systems (1999-07-12 : Denver, Colorado, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1999
- Summary:
- A transient thermal analysis of a Carbon/Carbon (C/C) Mars Entry Non-Ablative Aeroshell Assembly was performed to determine the maximum temperatures it would reach during a Mars entry. The purpose of this thermal analyses was to (1) determine the maximum temperatures of the 5 layers and the close-out which make up the aerothermal shield and (2) to transmit these temperatures from SINDA/G finite difference format to finite element format in COSMOS/M structures/dynamic models using Technical Alliance Group (TAG) developed SINDA/ G temperature translator software (STT)
- Notes:
- Vendor supplied data
- Publisher Number:
- 1999-01-2198
- Access Restriction:
- Restricted for use by site license
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