The objective of the research is to identify, develop and transition new propellants and advanced concepts for propulsion applications, such as hydrocarbon fuels for liquid boost, liquid and solid oxidizers for boost and upper stages, monopropellants for spacecraft and upper stages, cryogenic propellants for upper stages and laser light craft for microsatellite and other applications.
First Principles Calculations of Nitro Compounds with the A1 (111) Surface. DoD UGC, 10-14 Jun 02, Austin, TX
2002
26 pages
Report
Keine Angabe
Englisch
Basic & Synthetic Chemistry , Rocket Engines & Motors , Rocket Propellants , Propellants , Propulsion systems , Nitrogen compounds , Spacecraft , Boost phase , Liquids , Solids , Fuels , Hydrocarbons , Oxidizers , Transitions , Cryogenic propellants , Monopropellants , First principles calculations , Viewgraphs only
First-principles calculations of LaMnO3 surface reactivity
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