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Dynamic-model investigation of some landings and slideouts of a recoverable booster
Economy of large launch vehicles including orbital labor cost.
Effectiveness of external dampers for attenuating launch vehicle oscillations.
Effects and importance of penetration and growth of lift on space vehicle response
Egse for the post-saturn generation of launch vehicles.
Electrical support equipment for the saturn v launch vehicle system.
Electro-optical simulation of saturn spacecraft maneuvers final report, jun. 1964 - jan. 1965
Electrostatic measurement experiment, Scout Vehicle 131-R /S.E.V./
Emerging US Space Launch, Trends and Space Solar Power
Evaluation of maraging steel for application to space launch vehicles supplementary report
Evaluation of pilot's ability to stabilize a flexible launch vehicle during first-stage boost
Evaluation of pilot's ability to stabilize a flexible launch vehicle during first-stage boost
Evaluation of the Marc 7G1 auxiliary rocket motor for use on the Atlas-Centaur vehicle Final report
Experimental titanium crossbeam manufacturing technology Final report, 1 Jul. 1964 - 30 Oct. 1965
Explicit guidance equations for multistage boost trajectories
Feasibility and Design Study of an Unguided Solar Orbital Launch Vehicle
Feasibility of Large Launch Vehicle Recovery
Feasibility study of storage concepts for Scout and other NASA solid propellant launch vehicles
Fiber Optic Sensors for Launch Vehicles Project
Flight data display studies for real time computer flight evaluation Final report
Flight performance data from the scout x-258 rocket motor
Flight termination system for Centaur vehicle AC-6
Flow-field parameter analysis of the wind- induced oscillation of launch vehicles.
Flow field prediction and analysis study for project RAM B3 Final report
FLUID FLIGHT CONTROL SYSTEM ON TAP FOR SATURN