Performance of a turbojet combustor using natural gas fuel heated to 1200 F /922 K/
Turbojet combustor performance using natural gas fuel heated to 1200 F
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Turbojet combustor performance using natural gas fuel heated to 1200 F
Production and loss of O/1D/ in nighttime F region
Design, fabrication, and testing of antenna for ATS F and G synchronous satellites
Tests of magnetic materials from 800 to 1600 F
Ion chemistry and thermal balance in E and F region above Wallops Island
F region ionization and heating during magnetic storms
Preliminary lunar orbit attitude sequence for mission F
Determining test requirements for LM landing radar for F mission
Lunar module descent/phasing summary for mission F
Coherent propagation study proposal for ATS-F 10.6 micrometer laser communications experiment
Amplitude and phase variations of high frequency satellite signals transmitted through ionosphere F region
Oxygen collisional quenching rate in F region determined by comparing nightglow intensities with intensities calculated from electron density profiles
KCl F centers isothermal annealing kinetics using EPR, considering electron irradiation levels effects
Electrostatic drift-dissipative plasma instability and nocturnal equatorial spread F irregularities, discussing amplification in collision dominated medium
Electromagnetic drifts and neutral air winds effects on F 2 region derived from electron continuity equation, using Jacchia model atmosphere
Nickel base alloy, WAZ-20 with improved strength in 2000-2200 F range for application to gas turbine engine stator vanes
F-1 rocket engine acoustic liner, reevaluating damping data for combustion stability improvement
Script-F radiative interchange matrix for enclosures with arbitrary surface emission and reflection characteristics