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Radiation and Ablation Cooling for Manned Reentry Vehicles
Roberts, L.

Radiation and Ablation Cooling for Manned Reentry Vehicles

Author / Organization:
Aerospace & Aviation Published 2015 Verification Pending

Overview & Synopsis

The necessity of reducing heat transfer to reentry vehicles has led I to the consideration of both radiative and ablation shields. The paper reviews briefly the heating problems for manned vehicles and the means whereby ablation and radiation afford thermal protection. The principal energy disposal and weight parameters are then presented and their relation to the vehicle and trajectory parameters is discussed. A comparative analysis of three types of ablation shield is made and broad conclusions are drawn as to the type of shield most appropriate to manned reentry vehicles.

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Document Information

Document Title Radiation and Ablation Cooling for Manned Reentry Vehicles
Author / Organization Roberts, L.
Subject & Discipline OTHER
Categories Aerospace & Aviation
Publication Year 2015
License / Rights Public Domain / NASA STI Open Access
Resource Verification Listed PDF (Verification Pending)
Original Host Website NASA Technical Reports Server (ntrs.nasa.gov)
File Format application/pdf (Portable Document Format)
Language EN
Catalog ID DOC-75324
Original Source Link Visit Source Page on ntrs.nasa.gov »