Study of thermal conductivity requirements - MSFC 20-inch and 105-inch cryogenic tank analyses Interim report
Thermal analyzer computer program for venting cryogenic tanks
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Thermal analyzer computer program for venting cryogenic tanks
Flame inhibition and vapor release studied by microencapsulated fire retardant compounds
Minimum fuel attitude control of spacecraft by Pontryagin principle and extended steepest descent method
Velocity distribution in lower mantle, showing second major discontinuity in P wave travel time curve at 24 degrees
Advanced reconnaissance electric planetary spacecraft /AREPS/ concept for repeated coverage of Mars or Venus surface, using solar-photovoltaic system
Earth upper mantle wave velocity structure based on surface wave dispersion, noting low velocity layers thickness
Topologies introduced on state space for differential equations to obtain dynamical systems
D region ionizable constituent density /presumably nitric oxide/ measured, using blunt probe to detect changes in conductivity produced by Lyman alpha ionizing radiation
Basic theory of existence, uniqueness, and continuation for neutral functional differential equations
Exponential estimates and saddle point property for neutral functional differential equations
Cylindrical calorimeter designed to measure temperature dependent thermal conductivity for high performance insulation
Computerized analysis of thermal conductivity of 20-inch and 105-inch cryogenic space storage tanks
Thermal conductivity tests of high performance insulation for long term, space storage of cryogenic materials
Critical cases for neutral functional differential equations
Functional class of differential-difference, retard differential, and difference equations
Noncircular liquid rocket injector orifices and elements for liquid/liquid propellants
Uniform asymptotic stability of functional differential equations of neutral type
Advanced reconnaissance electric planetary spacecraft /AREPS/ concept for repeated coverage of Mars or Venus surface, using solar- photovoltaic system