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Reliable, Low Mass, Non-Invasive Pressure Transducers
Pegasus satellite measurements of meteoroid penetration, February 16 - December 31, 1965
Spread-f observations by the alouette topside sounder satellite
RECENT ADVANCES IN THE APPLICATION OF PHOTOELASTICITY IN THE MISSILE INDUSTRY
Power Measurements to Excavate Lunar Soil Simulant GRC-3B Using Arc Backhoe Trajectories
Development of magnetic test facilities at Goddard Space Flight Center
Pegasus satellite measurements of meteoroid penetration /February 16 - July 20, 1965/
Low level gas purged radiometer model no. R8100A, phase II. Final report
Detailed behavior of the midlatitude ionosphere from the explorer xvii satellite
Instrumentation report on nike apache flight 14.127 gi
In-Situ Geochronology as a Mission-Enabling Technology
A practical software measurement mechanism
A practical software measurement mechanism
Zero Mass, Packageless and Non-Invasive Pressure Transducer
Preliminary Results from Propellant Mass Gauging with Electrical Capacitance Tomography
The propagation of sound from airport ground operations
The feasibility of sea surface temperature determination using satellite infrared data
Comparison of pre-launch and flight vibration measurements on thor vehicles
Wake Measurements Behind a Wing Section of a Fighter Airplane in Fast Dives
Execution-Error Modeling and Analysis of the GRAIL Spacecraft Pair
CONFERENCE ON LUNAR EXPLORATION PART B. PROCEEDINGS
Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63
DRAG COMPENSATION AND MEASUREMENT WITH MANNED SATELLITESFEASIBILITY STUDY
A Miniaturized GC/MS Instrument for Space Flight Operations
Techniques for mounting an ultrasonic temperature device Final report
Thermophysical properties measurements performed for NASA
High-speed photography of aluminum particle combustion in flames.
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.
Surveyor III preliminary scientific results press briefing
Requirements for onboard optical guidance of spacecraft on lunar trajectories.
Design Optimisation and Mass Saving of the Structure of the Orion-MPCV European Service Module
Guidelines for Dynamic Environmental Criteria: An Invitatin to Participate in Their Development
1.5 million pound load cell calibration and H-area thrust measuring system Technology report
PROBLEMS OF ATMOSPHERIC WIND INPUTS FOR MISSILE AND SPACE VEHICLE DESIGN