Reusable Subsystems Design/Analysis Study. Volume III. Supplemental Data
Abstract
This volume provides supplemental data by way of appendixes to the task presented in Volume II AD-506 593, and AD-506 594. These appendixes include a Technology Summary, A Proposed Specification for Reusable Propulsion Components and Feed System, and Stress Analysis of Reusable Propellant Tanks. The Technology Summary presents a listing and information regarding previous technology programs in the areas of: integrated propulsion systems, cryogenic pressurization, cryogenic reaction control systems, propellant feed lines, liquid propellant tankage, propellant orientation and acquisition, inflight propellant conditioning, and space vehicle fluorine systems. The proposed specifications include a Proposed General Specification for Rocket Propulsion Fluid System Components and a Proposed General Specification for Rocket Propulsion Propellant Feed System, each obtained by modification of existing specifications. The stress analyses are presented for Reusable Launch Vehicle Propellant Tanks, Structural Analysis of Unsymmetric Fuel Tanks, and Symmetric Propellant Tanks.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1970
- Accession Number
- AD0506595
Entities
People
- H. K. Burbridge
- H. L. Jensen
- Lucian L. Morgan
- R. F. Hausman
- R. L. Gorman
Organizations
- Lockheed Martin Missiles and Space