PERFORMANCE AND SOME DESIGN ASPECTS OF THE FOUR-STAGE SOLIDPROPELLANT ROCKET VEHICLE USED IN THE RAM A1 FLIGHT TEST
Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performance and design
RADIO ATTENUATION↗
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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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Performance and operational characteristics of pentaborane fuel in 48-inch-diameter ram-jet engine
Combustion efficiency of pentaborane fuel in 48- inch diameter ramjet engine
RAMJET ENGINE↗
Investigation of an on-off inlet shock- position control on a 16-inch ram-jet engine
On-off inlet shock positioning equipment on 16 inch ramjet engine
INLET↗
Preliminary results from free-jet tests of a 48-inch-diameter ram-jet combustor with an annular can-type flame holder
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holder
FLAME HOLDER↗
Research study of some RAM antennas Final report, 18 Nov. 1964 - 18 Jun. 1965
Input impedance and radiation pattern determinations for cylindrical gap, waveguide excited and circular waveguide slot antenna arrays
ANTENNA ARRAY↗
Preliminary evaluation of flight-weight XRJ47-W-5 ram-jet engine at a Mach number of 2.75
Free jet investigation of performance, burner shell cooling, liner durability, and ignition characteristics of ramjet engine conducted in altitude test chamber at inlet Mach number 2.75
AERODYNAMIC CHARACTERISTICS↗
An analysis of high ionosphere positive ion ram probes
Analysis of rocketborne ion probe data from upper ionosphere, for planar and spherical probe geometries
UPPER IONOSPHERE↗
Theoretical flow field calculations for Project RAM
Flow field predictions for radio attenuation measurements on blunt reentry cone
Dresser, H.↗
Project RAM flight-test rocket vehicles
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Raper, J. L.↗
Results of the RAM B2 materials-addition flight experiment
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Cuddihy, W. F.↗
The RAM B3 reflectometer experiment
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Grantham, W. L.↗
RAM flight-test results and conclusions
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Schroeder, L. C.↗
Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine
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Meyer, C. L.↗
Design of combustor for long-range ram-jet engine and performance of rectangular analog
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Koch, R. G.↗
Altitude performance of a 20-inch-diameter ram-jet engine investigated in a free-jet facility at Mach number 3.0
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Smolak, G. R.↗
Effect of design changes of operating conditions on combustion and operational performance of a 28-inch diameter ram-jet engine
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Nakanishi, S.↗
Altitude free-jet investigation of dynamics of a 28-inch-diameter ram-jet engine
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Crowl, R. J.↗
Experimental investigation of diffuser pressure ratio control with shock positioning limit on 28 inch ram-jet engine
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Crowl, R. J.↗