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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.
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Role of proprioceptive impulses during respiration with increased intrapulmonary pressure in regulating respiration and circulation
Linear guidance equations for impulse velocity corrections in space missions
Mechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engine
Impulsive injection of electrons into earths inner trapping region from solar cosmic ray events
Impulsively started steady flow and uniformly accelerated unsteady flow about circular cylinders and mathematical models
Computational method for two impulse orbital transfer and rendezvous between two elliptical orbits
Patched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer trajectory
Minimum impulse time free transfer between elliptic orbits
Minimum fuel consumption two impulse soft lunar landing trajectories
Modifications of impulse approximation allowing for motion of bound electrons, providing simple analytic expressions for atomic ionization and detachment cross sections
Impulsive emission of approximately 40-kev electrons from Sun observed from Mariner IV
Worldwide positive-negative impulse pair observed on geomagnetic records found to be recurrent and associated with M-region disturbances
Numerical determination of optimum two-impulse orbital transfers between inclined elliptical orbits
Torque-free precession of spin stabilized spacecraft, showing thrust misalignment as cause for final burnout impulse
Improper random process where impulse occurrence times constitutes stationary point process, noting autocorrelation function and spectral density function
Propagation of nervous impulse down medullated and unmedullated fibers, obtaining expression involving ionic conductances
Monte Carlo simulation for adaptive policy for multiple impulse correction of trajectory of spacecraft
Adding soluble solid oxidizers to hydrazine and similar fuels makes them useful in low temperature bipropellant systems. These oxidizers improve the low specific impulse, high freezing point, low boiling point, and low density of the fuels.