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Messen
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Measurement of the earth's atmosphere Final report
A photomechanical investigation of the Algol solid propellant rocket motor nozzle Final report
Radar Studies of the Moon Quarterly Progress Report No. 3, 1 May - 31 Jul. 1966
Self-induced balloon motions and their effects on wind data
Development of instrumentation for measurement of bone density Final report
Project baldy- an investigation of aerodynamically-induced balloon motions final report
Simulated Versus Measured UHF Radiated Power at LaRC Street Level
The measurement of the surface temperature of the earth technical paper no. 64
The Design of a Skin Friction Meter for Use in Extreme Environmental Conditions Final Report
Description and analysis of 890-MHz noise-measuring equipment
Steady and fluctuating pressures at transonic speeds on hammerhead launch vehicles
Compendium of wind data from the vapor trail technique
Precision flow measurement techniques for low thrust auxiliary propulsion liquid rockets
Measurement of the UH-60A Hub Large Rotor Test Apparatus Control System Stiffness
Analysis and experimental verification of axial thrust on the M-1 liquid oxygen turbopump
Pegasus satellite measurements of meteoroid penetration /February 16 - July 20, 1965/
Low level gas purged radiometer model no. R8100A, phase II. Final report
Pegasus satellite measurements of meteoroid penetration, February 16 - December 31, 1965
Detailed behavior of the midlatitude ionosphere from the explorer xvii satellite
Instrumentation report on nike apache flight 14.127 gi
The feasibility of sea surface temperature determination using satellite infrared data
Survey of extraterrestrial non-solar X-radiation by rocket borne instruments Final report
Techniques for mounting an ultrasonic temperature device Final report
Thermophysical properties measurements performed for NASA
A feasibility study of an advanced space environmental effects sensor
Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing
Mass spectrometer for lunar analysis study Final summary report, 1 Jun. - 31 Aug. 1963
1.5 million pound load cell calibration and H-area thrust measuring system Technology report