MATERIAL AND PROCESSES R AND D REPORT, STORABLE TOROIDAL COMBUSTOR DEMONSTRATION PROGRAM. VOLUME 2
Abstract
Regenerative cooling feasibility demonstrations were accomplished at 2000-psia chamber pressure with a 10,000-pound-thrust toroidal combustor using storable propellants with nitrogen tetroxide as the coolant. The coolant passages of the toroidal combustor were fabricated from Hastelloy-X tube material. An epoxy resin sealer material was used in the joints between the contoured walls and the end plates of the combustor, thereby preventing high-pressure hot-gas leakage.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1966
- Accession Number
- AD0376654