Gas evolution from a solid rocket propellant during depressurization to produce a quench.
Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
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Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Photographic observations of rocket nightglow
Parachute for meteorological rockets, noting design, testing, high altitude performance, etc
RF transmission through plasmas created by rocket exhaust of Saturn vehicle
Metals for liquid propellant rocket systems in terms of environments in which performance is required
Techniques for rocket solar UV and for UV SPECTROSCOPY
Rocket and balloon-borne exposure study of terrestrial microorganism survival in space
Upper ionospheric electron density measurement by signals propagated between two parts of high altitude rocket
Rocket smoke-trail wind measurement technique
Seismograph used for measuring natural seismic activity and similar man-made disturbances like large rocket firings, showing propagation of disturbance by ground and not by atmosphere
Random noise effects and optimal control of nuclear rocket start-up for rapid and precise attainment of full power
Short duration simulation of rocket exhaust products, flow duration through nozzle and effect on recirculation flow fields
Propellant rocket exhaust plume effect on error calculation for radiation balance IR tracker
Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
Rocket-borne neutron detector measurements of neutron albedo and intensities at various geomagnetic latitudes
Acoustic absorption liners for suppressing HF COMBUSTION instability in rocket engine combustion chambers
Number densities of ions and electrons in D region measured, using Arcas rocket
Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines