Two-Stage-to-Orbit Spaceplane Concept with Growth Potential-Reference-Cited by-同舟云学术

Two-Stage-to-Orbit Spaceplane Concept with Growth Potential

Published:2001-11 Issue:6 Volume:17 Page:1149-1161
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Mehta Unmeel B.¹,Bowles Jeffrey V.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5886

Reference17 articles.

1. Augenstein, B. W., Harris, E. D., with Aroesty, J., Blumenthal, L., Brooks, N., Frelinger, D., Garber, T., Gottenmoeller, R., Hiland, J., Liu, S. K., Pace, S., Rosen, J., Rowell, L., and Stucker, J. “The National Aerospace Plane (NASP): Development Issues for the Follow-on Vehicle, Executive Summary,” RAND, R3878/1-AF, Santa Monica, CA, 1993.

Cited by 30 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of strut schemes on combustion characteristics in innovative combined ramjet engine;Acta Astronautica;2024-09

2. Heat transfer performance investigation of rotating U-channel supercritical pressure hydrocarbon fuel with intermediate connection section;International Communications in Heat and Mass Transfer;2023-11

3. Prospects for scramjet engines in reusable launch applications: A review;International Journal of Hydrogen Energy;2023-11

4. Trajectory Optimization of a Partially Reusable Rocket–Scramjet–Rocket Launch System Including Fly-Back;Journal of Spacecraft and Rockets;2023-05

5. Scramjet Intake Design Based on Exit Flow Profile via Global Optimization and Deep Learning toward Inverse Design;AIAA SCITECH 2022 Forum;2022-01-03