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Precision flow measurement techniques for low thrust auxiliary propulsion liquid rockets.
Mass flux and impact pressure probes for use in arcjet exhausts.
Remarks on the Interpretation of Lunik 10 Magnetometer Results
On the dynamic characteristics of a variable- mass slender elastic body under high accelerations.
Effect of Propellant Injection Through Electrodes on Potential Distribution in an MPD ARC
Secondary measurements by Pegasus
Radar Studies of the Moon Quarterly Progress Report No. 3, 1 May - 31 Jul. 1966
Sonic-boom measurements during bomber training operations in the Chicago area
The Design of a Skin Friction Meter for Use in Extreme Environmental Conditions Final Report
Compendium of wind data from the vapor trail technique
Description and analysis of 890-MHz noise-measuring equipment
The Goddard range and range rate tracking system - Concept, design and performance.
The dynamic environment of spacecraft surface transportation
Line spectra of delta and pi Scorpii in the far-ultraviolet.
Tests and combination of satellite determinations of the gravity field with gravimetry.
Radiative properties of carbon particles produced by a rocket motor.
Pegasus satellite measurements of meteoroid penetration, February 16 - December 31, 1965
Analysis and experimental verification of axial thrust on the M-1 liquid oxygen turbopump
Techniques for mounting an ultrasonic temperature device Final report
Requirements for onboard optical guidance of spacecraft on lunar trajectories.
1.5 million pound load cell calibration and H-area thrust measuring system Technology report
Additional comments on ''an inexpensive rocket technique for obtaining low level wind profiles.''
The predictability of winds and virtual temperature profiles for flight and static test operations.
A feasibility study of an advanced space environmental effects sensor
The feasibility of sea surface temperature determination using satellite infrared data
Survey of extraterrestrial non-solar X-radiation by rocket borne instruments Final report
Total boundary-layer mass flow with mass transfer at the wall.
Investigation of stresses in the Algol II-B ROCKET nozzle model Final technical report
Lunar orbiter - Tracking data indicate properties of Moon's gravitational field.
Flight research program. IV - A small gas analyzer for aerospace.