Field-enhanced Thermionic Emission from Electrodes of Cesium Ion Thrustor
Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine Or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction
Investigation of an Afterburning Ramjet Using Gaseous Hydrogen as Fuel at Mach Number of 3.0
Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Effect of Screens in Reducing Distortion and Diffusion Length for a "dump" Diffuser at a Mach Number of 3.85
Performance of a Short Hydrogen-fueled Ramjet at Mach Numbers of 3.2 and 3.6
Experimental Investigation of the Performance of a Mach-2.7 Two-dimensional Bifurcated Duct Inlet with 30 Percent Internal Contraction
A 5-centimeter-diameter Electron-bombardment Thrustor with Permanent Magnets
Design of a Very-low-bleed Mach 2.5 Mixed-compression Inlet with 45 Percent Internal Contraction
Distortion in a Full-scale Bicone Inlet with Internal Focused Compression and 45 Percent Internal Contraction
Performance of a 28-inch Ramjet Utilizing Gaseous Hydrogen at a Mach Number of 3.6, Angles of Attack Up to 12 Degrees, and Pressure Altitudes Up to 110,000 Feet
Performance of Vortex Generators in a Mach 2.5 Low-bleed Full-scale 45-percent-internal-contraction Axisymmetric Inlet
Boundary-layer Bleed System Study for a Full-scale, Mixed-compression Inlet with 45 Percent Internal Contraction
Performance and Surge Limits of a TF30-P-3 Turbofan Engine/axisymmetric Mixed-compression Inlet Propulsion System at Mach 2.5
Boundary Layer Bleed System for a Full-scale, Mixed Compression Inlet with 45 Percent Internal Contraction
Interaction of an Exhaust Jet and Elementary Contoured Surfaces Located in a Supersonic Air Stream
Interaction of a Jet and Flat Plate Located in an Airstream
Experimental and Analytical Investigation of the Dynamic Response of a Supersonic Mixed-compression Inlet
Field-enhanced Thermionic Emission from Electrodes of Cesium Ion Thrustor