Surface-protection and cooling systems for high-speed flight.

David J. Masson, Carl Gazley

ResearchPublished 1956

A discussion of systems for surface protection against transient and continuous heat inputs, corresponding to typical missile and aircraft flight paths. Comparisons of various systems are made for several typical operating conditions.

Document Details

  • Copyright: RAND Corporation
  • Availability: Web Only
  • Year: 1956
  • Pages: 44
  • Document Number: RM-1735

Citation

Chicago Manual of Style

Masson, David J. and Carl Gazley, Surface-protection and cooling systems for high-speed flight. Santa Monica, CA: RAND Corporation, 1956. https://www.rand.org/pubs/research_memoranda/RM1735.html.
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