NASA/SP-8014, Sherman*, M.M., Entry thermal protection, NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), *Philco-Ford Corporation, August,1968, pp. 37, Format(s): PDF 2252k |
Entry thermal protection, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
| Keywords: | reentry shielding, spacecraft reentry, systems engineering, thermal protection, ablative materials, film cooling, heat sinks, radiative heat transfer, space environment simulation, structural design, sweat cooling |
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| CASI Document ID Number: | 69N71545 |
| Subjects: | Engineering: Fluid Mechanics and Thermodynamics: Thermal Protection Astronautics: Launch Vehicles And Launch Operations: Reentry Vehicles |
| ID Code: | 9 |
| Deposited On: | 13 May 2002 |