DEVELOPMENT OF ULTRA-HIGH STRENGTH ROCKET MOTOR CASES BY CRYOGENIC STRETCH FORMING AND COOLED SOLID PROPELLANT ROCKET NOZZLES

Abstract

This report gives an account of progress for the period December 21, 1960 to January 20, 1961. The information is presented in two (2) sections. The first section describes the work performed on Task A, Development of Ultra- High Strength Rocket Cases by Cryogenic Stretch Forming. The second section reports progress on Task B, Cooled Solid Propellant Rocket Nozzles.

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Document Details

Document Type
Technical Report
Publication Date
Jan 20, 1961
Accession Number
AD0605138

Entities

People

  • R. H. Alper

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Contracts
  • Creep
  • Flow
  • Gas Turbine Nozzles
  • Hard Copy
  • Heat Transfer
  • Materials
  • New Jersey
  • Nozzles
  • Rocket Engines
  • Rocket Nozzles
  • Rockets
  • Solid Propellants
  • Stainless Steel
  • Stress Corrosion
  • Stretch Forming
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Metallurgy
  • Technical Research and Report Writing.