Accession Number : AD0283547

Title :   THRUST PROGRAMS FOR MINIMUM PROPELLANT CONSUMPTION DURING VERTICAL TAKE-OFF AND LANDING MANEUVERS OF A ROCKET VEHICLE IN A VACUUM

Corporate Author : BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH

Personal Author(s) : HULL,DAVID G.

Report Date : JUL 1962

Pagination or Media Count : 1

Abstract : D- 83 5479N > + T RU PROGR FOR I IMUM PROP LLANT CONSU P IO I V R IC L K -OFF AN LA I G OF ROCKET VEHICLES IN A VACUUM.

Descriptors :   *BOOSTER ROCKETS, *FUEL CONSUMPTION, ENERGY, ENERGY MANAGEMENT, EQUATIONS, GRAVITY, LANDING, MANAGEMENT ENGINEERING, MANEUVERABILITY, MATHEMATICAL ANALYSIS, THRUST, VACUUM APPARATUS, VERTICAL TAKEOFF AIRCRAFT, WEIGHTLESSNESS

Distribution Statement : APPROVED FOR PUBLIC RELEASE