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Grid fin
Validation of Wind Tunnel Test and Cfd Techniques for Retro-Propulsion (Retpro): Overview on a Project Within the Future Launchers Preparatory Programme (Flpp)
IAC-17-D2.4.3 Page 1 of 18 IAC-17
Supersonic Retropropulsion Wind Tunnel Testing
Spacex의 발사체 개발 전략 분석
07 270520 WAI Turns 1 by Stinger NSW
Multi-Disciplinary Design of a Grid Fin for a Generic High Speed Missile
Disrupting Launch Systems
Launch Vehicle First Stage Reusability a Study to Compare Different Recovery Optionslaunch Vehicle for Am
A Multidisciplinary Study on a VTVL and a VTHL Booster Stage
Space Launch Vehicle Design
JB3-2102 Design, Analysis, and Test of a High-Powered Model Rocket-2
재사용 우주발사체의 회수 기술 현황 및 분석 a Survey on Recovery
Stabilization and Control of a Vertically Landing Launcher
(ENTRAIN): a Multidisciplinary Study on a VTVL and a VTHL Booster Stage
Grid Fins As Efficient Control Surface in Comparison to Conventional Planar Fins
Design and Optimization of a Small Reusable Launch Vehicle Using Vertical Landing Techniques Stephane Contant Delft University of Technology
Preliminary Discussion Cost for a Rlv
Study of Launcher Recovery Systems
Top View
Grid Fins Shape Design of a Launch Vehicle Based on Sequential Approximation Optimization
Integration of Grid Fins for the Optimal Design of Missile Systems By
Design of a Grid Fin Aerodynamic Control Device for Transonic Flight Regime
Wiscwind U.S. Department of Energy Collegiate Wind Competition
Aerodynamics Analysis of Grid Fins Inner Lattice Structure in Cruise Missile