Analytical study of the use of visual references for thrust vector orientation in pilot-controlled lunar landings.
Thrust vector orientation during pilot controlled lunar landing with aid of visual references
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.
Thrust vector orientation during pilot controlled lunar landing with aid of visual references
Thrust vector control orientation during pilot controlled lunar landing with aid of visual references
Thrust vector control for solid propellant rocket engines - liquid injection system, hot or cold gas systems, and gimballed nozzle systems
Optimization of hydraulic thrust vector control systems for launch vehicles - component handbook
Vortex flow and erosion in rocket nozzles from warm-gas injection for thrust vector control
Simplified thrust vector orientation technique for establishing lunar orbits
Open-loop pulsed transfer functions of simplified thrust vector control system for Saturn-type vehicle with unsampled input derived by several methods
Analysis of sampled data digital compensated thrust vector control system
Determination of stability margins in channels of multiloop sampled data system, especially attitude channel of thrust vector control system
Feasibility of pneumatic digital actuator for thrust vector control
Design and performance characteristics of variable dynamic force vector rocket test apparatus
Discontinuous vector field stability and optimal feedback control
Pulsed transfer function of simplified thrust vector control system for Saturn-type vehicle
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial velocity vector
Irreducible unitary representations of restricted Lorentz group on manifolds of time-, light- and spacelike 4-vectors, obtaining plane-wave solutions of Klein-Gordon equation
Proportional hot gas secondary injection thrust vector control system for high energy solid propellant rocket motor
Vector analysis approach to algebra of rotations with applications to least-squares rotation and rigid body motion
Thrust vector deflection angle requirements for controlling solid propellant launch vehicle