Aerozine 50
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- Analysis of a Hybrid Propulsion Lunar Sample Return Mission
- Through Sclcncs DETERMINATION of T H E R M O M M C PROPERTIES of AERCEINE-50 Phase I Report 2 7 December 1966 to 27 January 1967
- Future of Space Travel
- U.S. Space Launch Vehicles Space Launch U.S
- A Reliable Method for Predicting the Specific Impulse of Chemical Propellants Dany Frem1
- Spacecraft Propulsion.Pdf
- Must Be a Real Engine Which Does Not Fire on Launchpad During Nominal Launch Sequence. No Launch System Engi
- U.S. Space Launch Systems
- A Liquid Propulsion Panorama
- CONSTRUCTION in Location
- RS-27A Rocketdyne Engine) - Lox/Kerosene, Mixture Ratio: 2.24:1
- Thermochemical Analysis of Hypergolic Propellants Based on Triethylaluminum/Nitrous Oxide
- TRW Pintle Engine Heritage and Performance Characteristics Gordon A
- A Summary of NASA and USAF Hypergolic Propellant Related Spills and Fires
- INVESTIGATION of the COMPATI Blllty of GOLD BRAZE ALLOYS with AEROZINE 50 Report 3332 8 November 1967
- The Road to the Moon Went Through Western New York
- Chemical and Plasma Rocket Propulsion
- Paper Session IB-US Expendable Liquid Rocket Propulsion