Ssme Alternate Turbopump Development Program: Design Verification Specification for High-Pressure Fuel Turbopump

By National Aeronautics and Space Administration

The design and verification requirements are defined which are appropriate to hardware at the detail, subassembly, component, and engine levels and to correlate these requirements to the development demonstrations which provides verification that design objectives are achieved. The high pressure fuel turbopump requirements verification matrix provides correlation between design requirements and the tests required to verify that the requirement have been met. Unspecified Center...

• Format: Paperback
• Language: English
• ISBN: 1730943837
• ISBN13: 9781730943836
• Release Date: January 1
• Publisher: Independently Published
• Length: 90 Pages
• Weight: 0.51 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"