Accession Number:

AD0842196

Title:

VEGA MODEL VORTEXING INVESTIGATION,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1960-08-04

Pagination or Media Count:

11.0

Abstract:

This report describes configurations tested to control fluid flow at tank outlet. The object of this test was to determine if vortexing would occur at the propellant tank outlet, and to develop and to test anti-vortexing devices if vortexing occurred. Author

Subject Categories:

  • Fluid Mechanics
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE