DEVELOPMENT OF A HIGH-TEMPERATURE, NUCLEAR RADIATION-RESISTANT PNEUMATIC POWER SYSTEM FOR FLIGHT VEHICLES
Abstract
The development of a high-temperature, nuclearradiation-resistant pneumatic power system for flight vehicles is considered. Future flight vehicles will be subjected to extreme thermal environments because of heat generated by supersonic speeds and/or the propulsion systems. This results in new requirements for components and auxiliary systems. It is, therefore contemplated to design, develop and test a typical pneumatic system capable of operating under wide temperature excursions while in the presence of nuclear radiation. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 24, 1962
- Accession Number
- AD0293879
Entities
Organizations
- General Dynamics