SPACE-CHARGE-FLOW THEORY AND ELECTRODE DESIGN FOR ELECTROSTATIC ROCKET ENGINES
Space charge-flow theory and electrode design for electrostatic rocket engines
ELECTRODE↗
SEARCH · Engineering Papers
Results for “Lockwood”
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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Design of a neutron monitor for measurements in space scientific report no. 1
Neutron detection system for space measurements
NEUTRON DETECTOR↗
High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-mounted horizontal tails
VARIABLE SWEEP↗
Low-speed wind-tunnel studies relating to pitch-up on a supersonic transport model with a high-aspect-ratio variable-sweep wing
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model for determining methods of reducing pitch-up tendency
PITCH CONTROL↗
Ground effects related to landing of airplanes with low-aspect-ratio wings
Influence of ground induced aerodynamic effects on landing maneuver of aircraft with low aspect ratio wings
AIRCRAFT LANDING↗
Neutron albedo measurements on rocket flights.
Rocket-borne neutron detector measurements of neutron albedo and intensities at various geomagnetic latitudes
EARTH ALBEDO↗
Effects of Reynolds number and flow incidence on the force characteristics of a family of flat-front cylinders
Reynolds number and flow incidence effects on cross flow characteristics of flat front, two- dimensional cylinders
CYLINDER↗
Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails
Low-speed characteristics of variable-sweep supersonic transport model with blended engine fuselage and engine-mounted tails
FLIGHT CHARACTERISTICS↗
A fast neutron-gamma detector for space research.
Test results on anticoincidence system for charged particle shield in fast neutron-gamma detector for space research applications
Lockwood, J. A.↗
Improved pulse shape discriminator for fast neutron-gamma ray detection system
Discriminator in nuclear particle detection system distinguishes nuclear particle type and energy among many different nuclear particles. Discriminator incorporates passive, linear circuit elements so that it will operate over a wide dynamic range.
Lockwood, J. A.↗
Research for the measuring of neutron intensity in space Final report
Measurements of neutron intensity and electron density in ionosphere
Lockwood, J. A.↗
Cosmic-ray neutron flux measurements above the atmosphere.
Cosmic ray neutron integrated flux measurements up to 350 km for energies to 15 Mev, determining neutron leakage flux
Friling, L. A.↗
Acoustic paramagnetic resonance in arsenic- doped germanium.
Acoustic paramagnetic resonance in arsenic doped germanium, measuring spin-lattice relaxation
Etzold, K.-F.↗
Apollo mission simulation with visual presentation.
Apollo mission simulation, discussing Command Module Simulator /CMS/, onboard computer system and dynamic visual presentation via infinity- optics display
Lockwood, L. W.↗
Cosmic ray neutron monitor for OGO-F.
OGO-F neutron monitor for measuring cosmic ray neutron flux near earth, locating sensor on boom to minimize spacecraft produced neutrons
Chupp, E. L.↗
Landing arrangement for aerial vehicles Patent
Aerospace configuration with low and high aspect ratio variability for high and low speed flight
Lockwood, V. E.↗
Landing arrangement for aerial vehicle Patent
Aerodynamic configuration for aircraft capable of high speed flight and low drag for low speed takeoff or landing upon presently existing airfields
Lockwood, V. E.↗
Landing arrangement for aerospace vehicle Patent
Aerospace vehicle with variable planform for hypersonic and subsonic flight
Lockwood, V. E.↗