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ANGELA : a new generation launcher : TIB Schlussbericht
On modeling and dynamics of a multiple launch rocket system
Dynamics design for multiple launch rocket system using transfer matrix method for multibody system
Abschlussbericht DIAMANT - Diaphragm Modelle, Analysen und Tests
Stern 2 : Abschlussbericht : Team Name Aquasonic II : experiment title: hybrid rocket
-Ferrocenedicarboxylic Acid Salts as Burning Rate Modifiers of Double-Base Propellant
DLR Reusability Flight Experiment ReFEx
Launch Dynamics Modeling and Simulation of Vehicular Missile System
On the Influence of Debris Landing Area Constraint on the Optimal Carrier Rocket Trajectory Design
Cost estimation for launch vehicle families considering uncertain market scenarios
Two-Stage Launch Vehicle Trajectory Modeling for Low Earth Orbit Applications
Effect of Initial State of Air-launch on Payload of Launch Vehicle
Ares I–X Flight Test Vehicle similitude to the Ares I Crew Launch Vehicle
New Launchers for Small Satellite Systems
Convex optimization of launch vehicle ascent trajectory with heat-flux and splash-down constraints
Convex Optimization of Launch Vehicle Ascent Trajectory with Heat-Flux and Splash-Down Constraints
Lyapunov based PD/PID in model reference adaptive control for satellite launch vehicle systems
Suggestions for a Roadmap towards Becoming a Launch Capable Nation
Low cost small-satellite access to space using hybrid rocket propulsion
Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control
Simultaneous Sizing of a Rocket Family with Embedded Trajectory Optimization
Robust adaptive backstepping control for reentry reusable launch vehicles
Adaptive control design for active Pogo suppression based on vibration-acceleration feedback
Genetic algorithm based parameter tuning for robust control of launch vehicle in atmospheric flight
Design aspects of launch vehicle sizing including air-breathing propulsion
Suboptimal reentry guidance of a reusable launch vehicle using pitch plane maneuver
The Design of Bolts Tighting Test System for Launch Vehicle Based on PLC and Servo Motor
Gas Permeation of Composites Subjected to Impact for Cryogenic Applications
Initial Orbit Determination Using Single Frequency GPS Measurements of Launch Vehicle
Optimal Launch Vehicle Configuration from Existing Solid Rocket Motors Using Genetic Algorithm
Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles
Dynamic analysis for vertical soft landing of reusable launch vehicle with landing strut flexibility
Effect of Reynolds Number and Aeroelastic Scaling Upon Launch-Vehicle Ground-Wind Loads
Development of Turbopump Systems for Cryogenic and Semicryogenic Propulsion Systems of ISRO
Global Three-Dimensional Emission Inventory for Launch Vehicles from 2009 to 2018
Hybrid adaptive ascent flight control for a flexible launch vehicle