SURFACE PRESSURE DISTRIBUTIONS ON 0.0628-SCALE MODELS OF PROPOSED PROJECT FIRE SPACE VEHICLES AT MACH NUMBERS FROM 0.25 TO 4.63
Surface pressure distribution on 0.0628 scale models of proposed project fire space vehicles
SEARCH · Search NASA
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.
Surface pressure distribution on 0.0628 scale models of proposed project fire space vehicles
Wind tunnel techniques used to determine pitch damping at large angles of oscillation for proposed mars atmospheric entry vehicles
Proposed units of length and time to facilitate coordination of space-time positions in orbital operations
Sonic boom characteristics of proposed supersonic and hypersonic aircraft
Diode and reactor design and nuclear fuels including uranium carbide alloys, uranium dioxide and uranium dioxide cermets for industry proposed in-pile thermionic space reactors
Laser method, where high energies of monochromatic light can be precisely collimated to perform welding and machining processes, is proposed for rotary dynamic balancing. The unbalance, as detected with the velocity pickup, would trigger the laser system which would emit high energy pulses directed at the heavy side of the component.
Reliability of proposed confidence level procedure for error probability of bank of correlations
Proposed landing sites for Apollo applications program lunar missions
Feasibility of nondestructive testing in space environment - proposed flight hardware for prototype nondestructive test unit
Retrodirective antennas and multipath transmission problems associated with use on proposed orbiting data relay network
Proposed test of theory of gravitation by an unshielded earth orbiting gyroscope using passive telemetry
Two proposed stabilization methods for X-15 horizontal surface control system
Proposed vertical alignment technique senses the attitude of a cranes cable and displays any deviation from the vertical. The system consists of a detector assembly fixed to the boom and a display scope located in the cabin. It has potential application with either fixed-boom cranes or gantries.
Cosmic dust experiment proposal for Pioneer F-G
Proposed contractual requirements to implement ultrahigh-reliability of parts for advanced planetary missions
Viscoelastic transitions and proposed liquid- liquid transition in polystyrene
Spectral reflectivity and emissivity observations of proposed Apollo landing sites compared with other lunar localities and unmanned lunar probe data
Lunar surface IR emissivity comparison spectra including proposed Apollo landing sites, indicating Si-O ratio difference for Plato crater