New Launchers for Small Satellite Systems
Development of Turbopump Systems for Cryogenic and Semicryogenic Propulsion Systems of ISRO
The Space Launch Services Industry: Indicators and Trends
Assessment and development of a ROM for linearized aeroelastic analyses of aerospace 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
Retrofitting and Redesigning of Conventional Launch Systems for Small Satellites
Issues and Perspectives on Space Launch Vehicles’ Development
Modeling of Martian Ascent Launch Vehicle
Modelling the Wall Pressure Fluctuations on the VEGA-C Launcher in Supersonic Conditions
The Aerospace Vehicle of the Future
How Will Sunsats Be Delivered to Space?
Sensitivity of Altitude Variation on Aerodynamics of a Typical Launch Vehicle During Hot Separation
Future Market for Space Transportation EUTELSAT’s Perspectives
Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
Long March Launch Vehicles — Responsive to both Domestic and International Market
Structural and Flow Analysis of Launch Vehicle for CubeSats
Global Launch Vehicle Systems for Potential Small Satellite Deployment
Economic and Technical Evaluation of Suborbital Spaceflight for Space Tourism1
Flight Safety System Operation During KSLV-I Flight
Reusable Launch Vehicles (RLVs) and Cost Engineering Principles
3D Guidance Algorithm for TAEM Phase Based on Coupling Coefficient
Combined satellite systems for continuous global coverage in equatorial and polar circular orbits
On the concept of a low-cost space system for detecting hazardous celestial bodies
Design Launch Vehicle Vertical Landing Guidance Law Using a Gauss Point Discrete Convex Programming
Launching Small Spacecraft — The Surrey Space Centre Experience
Integrated Guidance and Control Design for Orbit Injection Phase of Launch Vehicle
Time Domain Aero Control Structure Interaction Studies of Indian Reusable Launch Vehicle
Profiles of quick access to the orbital station for modern spacecraft
Reusables vs. Expendables: to Low Earth Orbit (LEO) and Beyond
Evolving Government Roles in an Increasingly Commercial Space Transportation Market
Fault-Tolerant Control for Launch Vehicle Actuator Based on Adaptive Control