NASA/SP-8062, Sherman*, M.M., Entry gasdynamic heating, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), *Philco-Ford Corporation, January,1971, pp. 60, Format(s): PDF 3339k |
Determining heat transfer to space vehicles entering planetary atmospheres for proper design and thermal protection
| Keywords: | thermodynamics, combustion, atmospheric entry, heat transfer, planetary, atmospheres, space capsules, thermal protection, aerospace engineering, flow distribution, gas dynamics, probability theory |
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| CASI Document ID Number: | 71N31179 |
| Subjects: | Engineering: Fluid Mechanics and Thermodynamics: Reentry Heat Transfer |
| ID Code: | 98 |
| Deposited On: | 15 May 2002 |