Development of a Zero-G Gauging System. Volume II.
Final rept. Oct 73-Jun 74,
TRW SYSTEMS GROUP REDONDO BEACH CALIF
Pagination or Media Count:
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.
- Liquid Rocket Propellants