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-Ferrocenedicarboxylic Acid Salts as Burning Rate Modifiers of Double-Base Propellant
Abort recovery strategy for future vertical landing systems
A comparison of iterative explicit guidance algorithms for space launch vehicles
Acoustic Characterization of Jet Interaction with Launch Structures During Lift-Off
Active Vibration Control of Launch Vehicle on Satellite Using Piezoelectric Stack Actuator
Adaptable Deployable Entry and Placement Technology Sounding Rocket One Modeling and Reconstruction
Adaptive control design for active Pogo suppression based on vibration-acceleration feedback
Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles
Adjusted Instantaneous Impact Point and New Flight Safety Decision Rule
Advanced GNC-oriented modeling and simulation of Vertical Landing vehicles with fuel slosh dynamics
Advanced modeling and trajectory optimization of the in-air-capturing maneuver for winged RLVs
Advancements in Mission Assurance Standards for Expendable and Reusable Launch Vehicles
Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
Aerospace launch vehicle control: an intelligent adaptive approach
A high assurance on-line recover technology for a space on-board computer
A lander mission to probe subglacial water on Saturn׳s moon Enceladus for life
Analysis and Optimization of Lunar Exploration Architecture Based on Reusable Human Spacecraft
Analysis of targeting method for closed-loop guidance of a multi-stage space launch vehicle
Analytical Investigation of Propellant Slosh Stability Boundary on a Space Vehicle
An approach for space launch vehicle conceptual design and multi-attribute evaluation
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
An indirect adaptive predictive control for the pitch channel autopilot of a flight system
A novel metamodel management strategy for robust trajectory design of an expendable launch vehicle
Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle
A reliable analytical navigation system based on symmetrical dynamic behavior of control channels
Ares I–X Flight Test Vehicle similitude to the Ares I Crew Launch Vehicle
Ares V launch vehicle: An enabling capability for future space science missions
A review of UK space activity and historiography, 1957–2007
Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension
A ring laser gyro based navigator for space launch vehicle guidance
A semi-expendable vehicle as RLV precursor