Minimization of SM RCS fuel for Skylab attitude maneuvers
Minimization of SM reaction control system for Skylab attitude maneuvers
Hough, W. W.↗
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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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The determination of attitude deviation limits for terminating a non-nominal translunar injection maneuver
Determining attitude deviation limits for translunar injection maneuver
Hyle, C. T.↗
A piloted simulator investigation of ground effect on the landing maneuver of a large, tailless, delta-wing airplane
Piloted simulator investigation of ground effect on landing maneuver of large, tailless, delta wing airplane
Drinkwater, F. J., III↗
Sonic boom propagation from maneuvering aircraft.
Sonic boom pressure signatures for uniform and maneuvering flight conditions determined for fighter and SST aircraft
Haefeli, R. C.↗
A zoom maneuver for descent of roll modulated entry vehicles
Flight maneuver for roll modulated lifting reentry vehicle to reduce deployment dynamic pressure
Staylor, W. F.↗
Loading conditions measured during aerobatic maneuvers
Loading conditions measured during aerobatic maneuvers in flight test to determine structural design requirements for aerobatic-type aircraft
Hall, A. W.↗
Dynamical equations for the plane change maneuver of the Lunar Hopping Laboratory
Dynamical motion of Lunar Hopping Laboratory in plane change maneuver between ballistic and foot-in-contact phases
Kaplan, M. H.↗
Helicopter rotor periodic differential pressures and structural response measured in transient and steady-state maneuvers
Helicopter rotor blade differential pressure and structural load characteristics in transient and steady state maneuvers
Ward, J. F.↗
Atmospheric maneuvers for space shuttles
Space shuttle atmospheric maneuvers, examining booster and orbiter entry, flyback and abort
Holloway, P. F.↗
Some trim drag considerations for maneuvering aircraft
Aft tail and canard configurations trim drag considerations for maneuvering aircraft
Dollyhigh, S. M.↗
Effects of the Valsalva maneuver on the cardiac systolic intervals - Beat-to-beat versus timed analysis
Valsalva maneuver beat-to-beat effects on systolic cardiac intervals compared with time based measurements
Flessas, A. P.↗
Hand-held self-maneuvering unit Patent
Hand-held maneuvering unit for propulsion and attitude control of astronauts in zero or reduced gravity environment
Huber, W. C.↗
Spacecraft attitude control during thrusting maneuvers - Space vehicle design criteria /Guidance and control/
Systems design criteria for spacecraft attitude control during thrusting maneuvers
Source record↗
Tracking and data system support for the Mariner Mars 1969 mission. Volume 2: Midcourse maneuver through end of nominal mission
Tracking and data system support for Mariner Mars 1969 mission from midcourse maneuver through end of nominal mission
Renzetti, N. A.↗
Solid-propellant motors for high-incremental velocity low-acceleration maneuvers in space
Low thrust long burning solid rocket propellant motor for orbit insertion maneuvers, discussing design, static tests, nozzle composition, igniter and performance
Shafer, J. I.↗
Space shuttle: Effect of orbiter/booster proximity interferences on the aerodynamic characteristics of the launch configuration during separation or abort maneuvers, M equals 0.6 - 1.38
The transonic phase of the 0.0088105-scale MSC orbiter booster separation test was conducted in the LTV 4-foot high speed wind tunnel, at Mach numbers of 0.6,0.9, 1.1, and 1.38. The purpose of this test was to define the effects of the orbiter/ booster proximity interference on the aerodynamic characteristics of the launch configuration during separation or abort maneuvers. Each model had both straight and delta wings available for variation of launch vehicle configuration concepts.
Romere, P. R.↗
Simulation of flight maneuver-load distributions by utilizing stationary, non-Gaussian random load histories
Random numbers were generated with the aid of a digital computer and transformed such that the probability density function of a discrete random load history composed of these random numbers had one of the following non-Gaussian distributions: Poisson, binomial, log-normal, Weibull, and exponential. The resulting random load histories were analyzed to determine their peak statistics and were compared with cumulative peak maneuver-load distributions for fighter and transport aircraft in flight.
Leybold, H. A.↗
Apollo experience report: Structural loads due to maneuvers of the command and service module/lunar module
Analyses were performed to determine the structural loads caused by maneuvers of the docked Apollo command and service module/lunar module (CSM/LM). Results of CSM/LM docked interface loads analyses and service-propulsion-system engine support structure load analyses are compared with the structural allowable loads of the CSM/LM docked interface and the service-propulsion-system engine thrust mount, respectively, for different phases of spaceflight operations. An analysis also was performed to investigate the loads that resulted from the failure case in which the LM descent propulsion system is started in the full-throttle position.
Rutkowski, M. J.↗