PROPELLANT UTILIZATION DIFFERENTIAL RATIO SYSTEM USING STANDARD PRESSURE SENSORS,

Abstract

A basic problem in Propellant Utilization is the achievement of a simple, reliable and rugged propellant sensor. This report describes a method of using inexpensive standard type pressure sensors to provide propellant mass ratio control. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 14, 1961
Accession Number
AD0675720

Entities

People

  • N. H. Kennedy

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Propellants
  • Standards

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Optical Fiber Sensing and Electromagnetic Propagation.
  • Rocket Propulsion.