Determination of Pressure Response Times for Gaseous Flow in a Tube

Abstract

The motivation for determining the response time for a pressure regulator to adjust the pressure at an area of interest located at the end of a long tube may be due to several reasons. One of these is the possibility that the regulator cannot be conveniently controlled from a more desirable position closer to the area of interest. Another reason to place to place the regulator a long distance from the area of interest might be to avoid high pressure lines over a prolonged distance. Consider the system shown in Figure 1, which is the proposed propulsion system for a microgravity experiment located in the Shuttle car bay. The regulator is controlled electronically so the ability to reduce the amount of electrical wiring will increase system reliability. Furthermore, Shuttle safety requirements demand that high pressure lines be tested for space worthiness, thus placement of the regulator close to the propellant source may eliminate the presence of these high pressure lines.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1993
Accession Number
ADA275274

Entities

People

  • Scott A. Baune

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Cold Gases
  • Computational Fluid Dynamics
  • Control Systems
  • Flow Rate
  • High Pressure
  • Mass Flow
  • Momentum
  • Poiseuille Flow
  • Pressure Regulators
  • Propulsion Systems
  • Regulators
  • Rocket Engines
  • Specific Heat
  • Specific Impulse
  • Supersonic Nozzles
  • Thrusters

Readers

  • Electrical Engineering
  • Robotics and Automation.
  • Theoretical Analysis.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Spacecraft Maneuvers