A mathematical model for defining explosive yield and mixing probabilities of liquid propellants.
Probability model for defining explosive yield and spill of liquid propellant
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Probability model for defining explosive yield and spill of liquid propellant
Yield and combustion physics of liquid propellant explosions determined from analytic charts
Large launch vehicle cryogenic propellant logistics including storage and production capacity optimization, cost and heat loss analyses by computer simulation
Flox-light hydrocarbon combinations desirable as liquid rocket propellants due to high specific impulse, hypergolicity and cooling properties
Solid propellant ignition and ignition propagation for rocket exhaust and hypergolic-type igniters
Solid rocket propellant quenching by depressurization, noting gas-side heat transfer coefficient
Cryogenic propellant boiloff losses in long duration space storage elimination by mechanical reliquefier, considering lunar, Earth-orbit and deep space application for hydrogen and oxygen
Microwave attenuation magnitude associated with exhaust plasma of nonaluminized and aluminized composite propellant
Liquid propellant reorientation experiments in tank models under low level acceleration
Gravitational stresses in circular cylindrical orthotropic viscoelastic solid propellant grain
Suitability of thermoplastic rubbers as binder for composite solid propellant
NASA-compiled bibliography with abstracts on high energy propellants, oxidizers, and related topics
High energy radiation methods for measuring liquid oxygen and liquid hydrogen mass in propellant tanks of orbiting spacecraft
Nonlinear aspects of combustion instability in liquid propellant rocket engines
Test firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
Ozone difluoride evaluated as liquid propellant additive
Flame propagation inside of cracks in polyester ammonium perchlorate composite propellants
Aluminum powder damping of HF instability in solid propellant combustion in vortex burner