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Structural and Flow Analysis of Launch Vehicle for CubeSats
Mathematical Model for the Separation Behavior of Low-Shock Separation Bolts
Pogo Stability Approaches for the Strap-On Launch Vehicle with Staged Combustion Cycle Engines
INFLUENCE OF INTERSTAGE DAMPING ON SATELLITE-LAUNCH VEHICLE LONGITUDINAL VIBRATIONS
Global Launch Vehicle Systems for Potential Small Satellite Deployment
Nuclear Thermal Propulsion for Jupiter and Saturn Rendezvous Missions
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Venting Analysis of the Payload Fairing of Korea Space Launch Vehicle II
Analytical Investigation of Propellant Slosh Stability Boundary on a Space Vehicle
Spacecraft Structure Model Validation and Test Philosophy
Modeling Space System Architectures with Graph Theory
System Exergy: System Integrating Physics of Launch Vehicles and Spacecraft
Computational-Fluid-Dynamics-Based Design Optimization of a Large Asymmetric Payload Fairing
Sounding rocket SS-520 as a CubeSat launch vehicle
Economic and Technical Evaluation of Suborbital Spaceflight for Space Tourism1
Coupled Fluid–Structure Interaction Analysis of Solid Rocket Motor with Flexible Inhibitors
Flight Safety System Operation During KSLV-I Flight
Analysis of targeting method for closed-loop guidance of a multi-stage space launch vehicle
Side Force Characteristics of Slender-Bodied Supersonic Vehicle with Two Protuberances
Reusable Launch Vehicles (RLVs) and Cost Engineering Principles
Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pyroshock of Satellite Separation
Path Planning Using a Novel Finite Horizon Suboptimal Controller
3D Guidance Algorithm for TAEM Phase Based on Coupling Coefficient
Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle
Rocket Noise Sources Localization Through a Tailored Beam-Forming Technique
Defining the Optimal Requirements for the Liquid Indium Microelectric Propulsion System
On the concept of a low-cost space system for detecting hazardous celestial bodies
Fluidic Thrust Shock-Vectoring Control: A Sensitivity Analysis
Rocket Landing Guidance Based on Linearization-Free Convexification
Highly Elliptical Rendezvous Orbits to Minimize Cryogenic Propellant Losses and Maximize Payload
Design Launch Vehicle Vertical Landing Guidance Law Using a Gauss Point Discrete Convex Programming
Statistical Entry, Descent, and Landing Performance Reconstruction of the Mars Science Laboratory
Parametric Analysis of Single-Stage Earth-Departure-Stage In-Orbit Refueling
Multidisciplinary Design Optimization of Waverider-Derived Crew Reentry Vehicles
Launching Small Spacecraft — The Surrey Space Centre Experience
Adaptable Deployable Entry and Placement Technology Sounding Rocket One Modeling and Reconstruction
Combined satellite systems for continuous global coverage in equatorial and polar circular orbits