X-33 trajectory optimization and design-Reference-Cited by-同舟云学术

X-33 trajectory optimization and design

Published:1998-08-10 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference and Exhibit
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Author:

Hill Ashley¹,Anderson David²,Coughlin Dan²,Chowdhry Rajiv³

Affiliation:

1. Sverdrup Technology, Inc., Huntsville, AL

2. NASA, Marshall Space Flight Center, Huntsville, AL

3. Lockheed Martin Skunk Works, Palmdale, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4408

Reference7 articles.

1. "X-33Aerospike Engine Operating Constraints andPReferences", Rev.5.0, August28,1997.

2. MichaelA MichaelB MichaelC Michael D MichaelE 236 386 386 344 344 233.71 204.61 204.61 196.80 196.80 8.72 10.23 10.23 10.30 10.29 183,754 189,673 190,242 179,420 179,426 14.11 28.61 22.29 24.65 27.33 4705 6002 5308 6376 6003 2.26 2.72 2.90 3.49 2.65 4000 6000 8000 10000 12000 Velocity (ft/sec)

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