CALIBRATION OF ELBOW FLOW METER FOR LIQUID OXYGEN VENT SYSTEM,

Abstract

This report describes the flow calibration of the 6 3/8-inch oxidizer vent system for the RTS phase 3 missile. The vent system was calibrated with gaseous oxygen at flows ranging from 4 to 16 lb/sec. A flow equation for the vent system has been developed from the calibration data and is shown in the results. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1959
Accession Number
AD0832068

Entities

People

  • S. J. Trizinsky

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Calibration
  • Cryogenic Propellants
  • Energetic Materials
  • Equations
  • Laboratory Procedures
  • Liquid Oxygen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Mathematics

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.