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launch vehicle
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Editorial : Enabling the Dream of Flight
Software Infrastructure for an Autonomous Ground Vehicle
Rocket Noise Sources Localization Through a Tailored Beam-Forming Technique
Compression Response of Fluted-Core Composite Panels
Mass and Cost Model for Selecting Thruster Size in Electric Propulsion Systems
Requirements Analysis of Propulsion Systems for Lunar-Exploration Mission
Instantaneous Impact Point Prediction Using the Response-Surface Method
Robust Reentry Guidance of a Reusable Launch Vehicle Using Model Predictive Static Programming
Computational-Fluid-Dynamics-Based Design Optimization of a Large Asymmetric Payload Fairing
Path Planning Using a Novel Finite Horizon Suboptimal Controller
Highly Elliptical Rendezvous Orbits to Minimize Cryogenic Propellant Losses and Maximize Payload
Quantitative Assessment of Multidisciplinary Design Models for Expendable Launch Vehicles
Standard Deviation of Launch Vehicle Vibration and Acoustic Environments
Precision Landing at Mars Using Discrete-Event Drag Modulation
Operational Modal Analysis of a Solid Rocket Motor from Firing Test
Design of an Airbreathing Second Stage for a Rocket-Scramjet-Rocket Launch Vehicle
Systems Architecting Methodology for Space Transportation Infrastructure
Effect of Spike Truncation on the Acoustic Behavior of Annular Aerospike Nozzles
Numerical Base Heating Sensitivity Study for a Four-Rocket Engine Core Configuration
Hot-Flow Simulation of Aeroacoustics and Suppression by Water Injection During Rocket Liftoff
Modeling Space System Architectures with Graph Theory
Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pyroshock of Satellite Separation
Statistical Entry, Descent, and Landing Performance Reconstruction of the Mars Science Laboratory
Parametric Analysis of Single-Stage Earth-Departure-Stage In-Orbit Refueling
Temporal Wind Pairs for Space Launch Vehicle Capability Assessment and Risk Mitigation
Prediction of In-Flight Radio Frequency Attenuation by a Rocket Plume
Mach Hydrocarbon-Fueled Scramjet Flight Experiment: The HIFiRE Flight 2 Project
Orbit Injection Considerations for Cluster Flight of Nanosatellites
Control Allocation of Reaction Control Jets: Quantization and Stability
Robust Predictive Control of a Class of Nonlinear Systems
Study on Acoustic Prediction and Reduction of Epsilon Launch Vehicle at Liftoff
Verification and Validation Framework for Autonomous Rendezvous Systems in Terminal Phase
Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle
Defining the Optimal Requirements for the Liquid Indium Microelectric Propulsion System
Prediction of Acoustic Loads on a Launch Vehicle: Nonunique Source Allocation Method
Effects of Shear-Layer Reattachment on the Nozzles of a Launch Vehicle
Launch Vehicle Base Flow Analysis Using Improved Delayed Detached-Eddy Simulation
Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension
Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept
Multidisciplinary Design Optimization of Waverider-Derived Crew Reentry Vehicles
Adjusted Instantaneous Impact Point and New Flight Safety Decision Rule
Improved Formulation for Predicting the Load Capacity of Marman Clamps
Effect of Freestream–Plume Interaction on Launch Vehicle Aerodynamics
Skylon Aerospace Plane and Its Aerodynamics and Plumes
Operational Methodology for Large-Scale Deployment of Nanosatellites into Low Earth Orbit
Time-Varying Structural Reliability of Launch Vehicle via Extreme Response Approach
Launch Dynamics Modeling and Simulation of Vehicular Missile System