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Analysis of Transportation Systems for Space Station Logistics
Analysis of triboelectric charging of launch vehicle fairings
Analytical and experimental studies of the dynamics of launch vehicles.
Analytical Investigation of Propellant Slosh Stability Boundary on a Space Vehicle
Analytical Study of Launch Vehicle Component Level Simulation, 26 March - 26 November 1965
Analytical study of launch vehicle component level simulation, 26 March - 26 November 1965
An analysis of aeroelastic divergence in unguided launch vehicles
An Analysis of Aeroelastic Divergence in Unguided Launch Vehicles
An analysis of chemical upper stages for nasa scientific missions
AN ANALYSIS OF THE CONING MOTIONS OF THE FINAL STAGES OF THREE NASA SCOUT DEVELOPMENT VEHICLES
An Analytical Investigation of the Effects of Stator Airfoil Clocking on Turbine Performance
AN APPLICATION OF TIME OPTIMAL CONTROL TO A FLEXIBLE LAUNCH VEHICLE
AN APPLICATION OF TIME OPTIMAL CONTROL TO A FLEXIBLE LAUNCH VEHICLE
An approach for space launch vehicle conceptual design and multi-attribute evaluation
ANDØYA SPACEPORT - EUROPE'S LAUNCH FACILITY FOR SMALL SATELLITES
AN EFFECTIVE PISTON PRESSURIZATION SYSTEM FOR SPACECRAFT BIPROPELLANT TANKS
An Electric Propulsion System to Reach a Geostationary Orbit
An evaluation of the whole-spacecraft passive vibration isolation system
A new analytical model for reliability analysis of a launch vehicle system with limited test data
A NEW CONCEPTUAL SCHEME FOR AIR LAUNCH REUSABLE LAUNCH VEHICLE (ALRLV)
A New Economic Concept for European Satellite Launch Vehicle Systems
A New Evolved Acceleration Reentry Guidance for Reusable Launch Vehicles
A NEW WEB-BASED KNOWLEDGE REPOSITORY OF THE WORLD'S LAUNCH SYSTEMS AND PROGRAMS
A NEW WEB-BASED KNOWLEDGE REPOSITORY OF THE WORLD’S LAUNCH SYSTEMS, PROGRAMS
AN EXPLORATORY STUDY ON THE POSSBBILITY OF THE SMALLSAT LAUNCH SERVICE IN S. KOREA
Angara and the Market for Non-Geostationary Orbit (NGSO) Satellites
ANGELA : a new generation launcher : TIB Schlussbericht
An indirect adaptive predictive control for the pitch channel autopilot of a flight system
An Industry Perspective of the Appropriate Role of the US Government in Future Space Transportation
AN INNOVATIVE NAVIGATION SCHEME FOR REUSABLE LAUNCH VEHICLE USING MULTI-SOURCE INFORMATION FUSION
Annual Report for 1967 to the Council of Europe
An Open Integrated Electronic System Software Architecture Design for Launch Vehicle
An Optimized Trajectory for a Two-Stage, Surface to Orbit Titan Launch Vehicle
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle
A NOVEL DESIGN APPROACH FOR A REUSABLE VTOL MICRO LAUNCH VEHICLE
A novel metamodel management strategy for robust trajectory design of an expendable launch vehicle