Accession Number:

ADA001668

Title:

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

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:

37.0

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. Contents include the following Flight test article general system description Test objective Test description Assembly and installation general System operation Conduct of the flight tests Data reduction Radiation safety mandatory reading.

Subject Categories:

  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE