FEASIBILITY DEMONSTRATION OF ADVANCED ATTITUDE CONTROL SYSTEMS.
Abstract
The period was devoted to accomplishing the following work for Task 1 - Completion of testing of the single coaxial injector configuration fabrication, assembly and testing of the multiple coaxial injector configuration and selection for thrust chamber durability testing, modification of one bipropellant valve to eliminate a flow choking condition, and preparation of the tungsten coated thrust chamber for welding to the multiple coaxial injector. Task 2 - Leak and gas volume checks of the fuel and oxidizer bellows pumps, assembly completion of the second heat exchanger, completion of the test setup for injector checkout tests, and initiation of injector tests with the single coaxial injector.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1966
- Accession Number
- AD0375465
Entities
People
- L. Montanino
- W. Pearson
Organizations
- Bell Aircraft Corporation