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-Ferrocenedicarboxylic Acid Salts as Burning Rate Modifiers of Double-Base Propellant
3D Guidance Algorithm for TAEM Phase Based on Coupling Coefficient
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
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
Aerospace launch vehicle control: an intelligent adaptive approach
A Japanese Road Map for Future Space Transportation System
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
Angara and the Market for Non-Geostationary Orbit (NGSO) Satellites
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 Open Integrated Electronic System Software Architecture Design for Launch Vehicle
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