A Laser-Ablation-Based Micro-Rocket.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA Plasmadynamics and Lasers Conference
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-2152
- Paper no.:
- 2002-2152
- Pages:
- 7
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
SPIE-The International Society for Optical Engineering |
SPIE - The International Society for Optical Engineering |
SPIE-The International Society for Optical Engineering |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Giant Momentum Coupling Coefficients from Nanoscale Laser-Initiated Exothermic Compounds
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Inlet Development for a Rocket Based Combined Cycle, Single Stage to Orbit Vehicle Using Computational Fluid Dynamics
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Plasma Generation and Plume Expansion for a Transmission-Mode Micro-Laser Plasma Thruster
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics
American Institute of Aeronautics and Astronautics |
SPIE - The International Society of Optical Engineering |
American Institute of Aeronautics and Astronautics |