Analyses for Turbojet Thrust Augmentation with Fuel-rich Afterburning of Hydrogen, Diborane, and Hydrazine
Turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine
DIBORANE↗
SEARCH · Engineering Papers
Results for “THRUST”
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.
Digital compensation of the thrust vector control system
Pulsed transfer function of simplified thrust vector control system for Saturn-type vehicle
DIGITAL COMPUTER↗
Modification to government-owned thrust stand system
Improvements in electric subsystem and capacity of thrust stand system for testing chemical, subliming, and cold gas thrustors
ELECTRIC CONTROL↗
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
OPTIMAL CONTROL↗
Perturbation solutions for low-thrust rocket trajectories.
Perturbation solutions of differential equations of motion for low-thrust rocket trajectories
PERTURBATION THEORY↗
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
OPTIMAL CONTROL↗
Burnout impulse may be thrust misalignment in disguise.
Torque-free precession of spin stabilized spacecraft, showing thrust misalignment as cause for final burnout impulse
THRUST EFFECT↗
Low-thrust trajectory and payload analysis for solar system exploration.
Trajectory energy requirements for low-thrust flights throughout solar system using nuclear- electric propulsion
TRAJECTORY ANALYSIS↗
A general method for determining optimum thrust nozzle contours for chemically reacting gas flows.
Optimum thrust nozzle contours for chemically reacting gas flows, obtaining set of partial differential equations for gas dynamic properties
GAS DYNAMICS↗
Low-thrust Trajectory Capabilities for Exploration of the Solar System Using Nuclear Electric Propulsion
Low-thrust trajectory requirements for solar system exploration using nuclear electric propulsion
NUCLEAR-ELECTRIC PROPULSION↗
Proportional solid propellant secondary injection thrust vector control study
Proportional hot gas secondary injection thrust vector control system for high energy solid propellant rocket motor
PROPORTIONAL CONTROL↗
An analysis of experimental data on entrance effects in circular thrust bearings
Empirical method for considering entrance effects in computing flow rates and load capacities of circular thrust bearings
THRUST BEARING↗
Transient and steady performance of an ion rocket thrust augmentor Summary report
Transient and steady performance of ion rocket thrust augmentor
IONIC PROPULSION↗
Thrust vector control requirements for solid- propellant launch vehicles
Thrust vector deflection angle requirements for controlling solid propellant launch vehicle
THRUST VECTOR CONTROL /TVC/↗
Error analysis of celestial-inertial navigation for low-thrust interplanetary vehicles
Error analysis of celestial-inertial navigation for low thrust electrically propelled interplanetary space vehicles
INERTIAL NAVIGATION↗
A study of low-thrust guidance
Mathematical statement and computer simulation of low thrust guidance problem - minimum time solutions
LOW THRUST PROPULSION↗
Optimum thrust nozzle contours for chemically reacting gas flows
Supersonic rocket nozzle design for optimum thrust with chemically reacting gas flows
GAS FLOW↗
The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitude
TRAJECTORY OPTIMIZATION↗