Accession Number:

ADA001667

Title:

Development of a Zero-G Gauging System. Volume II.

Descriptive Note:

Final rept. Oct 73-Jun 74,

Corporate Author:

TRW SYSTEMS GROUP REDONDO BEACH CALIF

Personal Author(s):

Report Date:

1974-09-01

Pagination or Media Count:

78.0

Abstract:

A configuration of the nucleonic gauging system denoted the Flight Test Article, which is suitable to demonstrate gauging performance in a zero-g environment as provided by the Zero-G KC-135 aircraft flying a parabolic trajectory, was designed, fabricated, and delivered to NASA. The gauging system is projected to yield a total system accuracy of 0.25 percent of total tank capacity with a 1-second response time. This volume contains the drawings and schematic diagrams.

Subject Categories:

  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE