Determination of the Effects of Acceleration-Induced Loads on a Propellant System Bladder.

Abstract

Four sections of propellant system bladders were evaluated during five tests on the 1-15 Test Area Centrifuge. Two specimens were accelerated to 25 g applied laterally to the test item and two specimens were accelerated to 20 g applied longitudinally. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1969
Accession Number
AD0862748

Entities

People

  • John Denker

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Centrifuges
  • Energetic Materials
  • Laboratory Equipment
  • Materials
  • Propellants

Readers

  • Brain and Cognitive Science; Experimental Psychology; Cognitive Neuroscience
  • Rocket Propulsion.
  • Structural Dynamics.