THE HEAT BARRIER,

Abstract

In a discussion of the heat barrier, the author first explains how this heat is produced. He notes that the problem was first discovered by the Germans in their experiments with V-2 rockets. He then describes the methods used to solve the problem. There are essentially two approaches to carry away the heat: by absorption and by radiation. The absorption techniques include: (1) Cooling by convection; the aircraft or rocket has a double wall with a gas or a liquid cooling agent in between to absorb the heat; (2) Cooling by evaporation; liquid is ejected from tiny holes punched in the wall of the aircraft; (3) Cooling by conduction; a thick shield is used and the heat is conducted away; (4) The burnout device; a protective layer is mounted on the craft; high temperature melts and burns this layer or starts a chemical reaction which absorbs large quantities of heat. The radiation technique uses an insulator which has a high radiation power. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 21, 1967
Accession Number
AD0674396

Entities

People

  • Wei Yeh

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Absorption
  • Aircrafts
  • Chemical Reactions
  • Convection
  • Cooling
  • Dielectrics
  • Evaporation
  • Heat Energy
  • High Temperature
  • Liquid Cooling
  • Radiation
  • Republic
  • Transition Temperature

Readers

  • Fluid Dynamics.
  • Materials Science
  • Spectroscopy.

Technology Areas

  • Microelectronics
  • Microelectronics - Graphene