Investigations for Missile Launching in an Improved Concentric Canister Launcher
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33274
Reference8 articles.
1. Concentric Canister Launcher
2. Concept analysis and laboratory observations on a water piercing missile launcher
3. Thruster Plume Surface Interactions: Applications for Spacecraft Landings on Planetary Bodies
4. Unsteady Gasdynamics Effects in Pyrotechnic Actuators
5. Experimental and Numerical Investigations of Flow Confined in a Vertical Missile Launcher
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