Gaseous hydrogen requirements for the discharge of liquid hydrogen from a 1.52 meter /5 ft/ diameter spherical tank
Physical parameter effect on pressurant gas requirements during expulsion of liquid hydrogen from spherical tanks
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Physical parameter effect on pressurant gas requirements during expulsion of liquid hydrogen from spherical tanks
Hydrogen gas pressure requirements during pressurization and transfer of liquid hydrogen from spherical tanks
Statistical effects of wind and atmospheric turbulence on launch vehicles
Electrical output transducer for measuring angular displacements does not introduce frictional contact between stationary and moving parts. It produces output voltages directly proportional to small rotary shaft displacements.
Peak wind probabilities for atmosphere over Cape Kennedy launching base
Design and performance of evaporator for vacuum ultraviolet mirror coatings by aluminum compound films
Gaseous-helium requirements for discharge of liquid hydrogen from 5-ft diameter spherical tank
Vacuum interferometer strain gage for absolute earth strain measurement via length change comparison with wavelength standard
Helium gas requirements for liquid hydrogen expulsion from spherical tank
Statistical analysis of wind distribution probabilities at Cape Kennedy
Real gas corrections to gas flow computations for sonic nozzles
Determination of low speed jet noise from fan engine for simulated nacelle configuration
Voltage range selection apparatus for sensing and applying voltages to electronic instruments without loading signal source
Electronic recording system for spatial mass distribution of liquid rocket propellant droplets or vapors ejected from high velocity nozzles
Flowmeters for sensing low fluid flow rate and pressure for application to respiration rate studies
Methods for determining mass flow rates of gases for use in calibrating gas flowmeters
Low hygrometer calibration for water vapor measurements smaller than 3 mm
Real gas mass flow rate computation through sonic nozzle