Phase I. Design and Analysis of Short Length Super HIPPO Motor Assembly.

Abstract

The short length Super HIPPO motor is a single cartridge version of the Super HIPPO high pressure ballistic test motor. The motor operates at pressures to 2,500 psi with propellant charge weights to 24,500 lb and is used to test rocket motor nozzles and components. This report summarizes the design and analysis activities, phase I, of a contract to design, fabricate, and install at AFRPL. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1977
Accession Number
ADA046083

Entities

People

  • P. R. Scannell
  • W. A. Stephen

Organizations

  • United Technologies Corporation

Tags

DTIC Thesaurus Topics

  • Air Force
  • Burning Rate
  • Combustion
  • Convection
  • Frequency
  • Heat Flux
  • Heat Transfer
  • Heat Transfer Coefficients
  • Ions
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Propellant Grains
  • Rocket Engines
  • Stress Analysis
  • Structural Analysis
  • Test Fixtures

Readers

  • Rocket Propulsion.
  • Software Engineering