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Low frequency analysis of rocket engines using compressible propellants

Pedestal-type calorimeter measures gamma-ray heating rates from 0.5 to 7.0 watts per gram of aluminum. Nuclear heating rate is a function of cylinder temperature change, measured by four chromel-alumel thermocouples attached to the calorimeter, and known thermoconductivity of the tested material.

Apollo Logistics Support Systems report on television systems for lunar mobile laboratory /Molab

Design considerations for integration of turbofan engine with reduced noise output in jet aircraft

Solid propellant rocket systems design and combustion efficiency and burning rate of solid propellants

Camera tube evaluations, earth station design, and television modification for lunar mobile laboratory /Molab/ - Apollo Logistic Support System