Super Loki Dart meteorological rocket system Final report
Design and flight test data on Super Loki Dart sounding rocket system for obtaining high altitude wind profiles with low cost rocket vehicle and radar-reflective chaff payload
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Design and flight test data on Super Loki Dart sounding rocket system for obtaining high altitude wind profiles with low cost rocket vehicle and radar-reflective chaff payload
Optimal thrust programming of single stage rocket vehicle for maximum payoff at end conditions using Lagrange multipliers for singular arc
Onboard computer equations for rocket vehicle guidance to elliptical orbit, discussing iteration absence from computations and digital simulation results
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit target
Ballistically effective atmospheric parameters for rocket vehicle design manuals involving application of climatological concepts of meteorology
Branched trajectory optimization for split rocket vehicles using projected gradient or steepest descent method
Gaseous nuclear rocket technology studies for application to nuclear engines for rocket vehicles
Flight performance of high resolution spectrometer in Aerobee rocket vehicle
Optimal control for rocket vehicle in three dimensional central force field
Attitude and propellant flow control system for liquid propellant rocket vehicles
Many liquid-propellant rocket vehicles have experienced longitudinal vibration, nicknamed pogo after the jumping stick, due to an instability arising from interaction of the vehicle structure with the propulsion system. These vibrations can produce an intolerable environment for astronauts and equipment, can overload vehicle structure, and can lead to loss of propulsion performance. A NASA monograph concerned with the prevention of pogo is well on its way toward publication and should serve as a useful guide to design for the Space Shuttle. The paper will briefly describe the nature of the pogo phenomenon, present a summary of past instabilities, relate the possible deleterious effects of pogo, and discuss the contents of the design criteria monograph. Finally, research tasks are recommended for support of pogo development activities on the Space Shuttle.
Hydraulic support equipment for full scale dynamic testing of large rocket vehicle under free flight conditions
Branched trajectory optimization for split rocket vehicles using projected gradient or steepest descent method
Rocket vehicle flight optimization for model including rigid body degrees of freedom in boundary layer approximation to attitude transients
Atmospheric ascent optimal trajectories for medium to high lift drag ratio space shuttle type rocket vehicles
Quick-release coupling for fueling rocket vehicles with cryogenic propellants
Remotely actuated quick disconnect for tubular umbilical conduits used to transfer fluids from ground to rocket vehicle
Rust prevention in stainless steel fluid transmission lines of nuclear engine for rocket vehicles