Reusable Launch of Small Satellites Using Scramjets
A new analytical model for reliability analysis of a launch vehicle system with limited test data
Unsteady Surface Pressure Characterization on Launch Vehicle in Liftoff Configuration
Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle
Hybrid optimization approach for rapid endo-atmospheric ascent trajectory planning
Ares V launch vehicle: An enabling capability for future space science missions
Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension
Evaluation of Exergy Efficiency Optimization of Space Launch Vehicles
Computational Assessment of the Efficiency of Using Various Fuel Pairs Onboard a Small Spacecraft
Impact of Geographical and Logistics Considerations on the Life Cycle Assessment of Launch Vehicles
Predefined-time control for a horizontal takeoff and horizontal landing reusable launch vehicle
Requirements Analysis of Propulsion Systems for Lunar-Exploration Mission
Retrofitting and Redesigning of Conventional Launch Systems for Small Satellites
Robust launch vehicle’s generalized dynamic inversion attitude control
Issues and Perspectives on Space Launch Vehicles’ Development
Uncertainty Quantification of Artemis I Space Launch System Integrated Aerodynamics Databases
An indirect adaptive predictive control for the pitch channel autopilot of a flight system
Comparison of Corcos-Based and Experimentally Derived Coherence Factors for Buffet Forcing Functions
Active Vibration Control of Launch Vehicle on Satellite Using Piezoelectric Stack Actuator
Modelling the Wall Pressure Fluctuations on the VEGA-C Launcher in Supersonic Conditions
The Aerospace Vehicle of the Future
Technologies of reducing the technological environmental impact of space rocket launches
Reviews and Challenges in Reliability Design of Long March Launcher Control Systems
Advancements in Mission Assurance Standards for Expendable and Reusable Launch Vehicles
Hot-Flow Simulation of Aeroacoustics and Suppression by Water Injection During Rocket Liftoff
How Will Sunsats Be Delivered to Space?
Editorial : Enabling the Dream of Flight
PCE-Based Robust Trajectory Optimization of Launch Vehicles via Adaptive Sample and Truncation
High-Precision Adaptive Predictive Entry Guidance for Vertical Rocket Landing
Optimal Mission Design for Moon Exploration Expedition
An Algorithm for Increasing Performance of a Space Launch Vehicle Using Solid Rocket Boosters
Sensitivity of Altitude Variation on Aerodynamics of a Typical Launch Vehicle During Hot Separation
Maximum-range trajectories for an unpowered reusable launch vehicle