Longitudinal Aerodynamics of a Winged Reentry Vehicle at Supersonic Speed-Reference-Cited by-同舟云学术

Longitudinal Aerodynamics of a Winged Reentry Vehicle at Supersonic Speed

Published:2018-09 Issue:5 Volume:55 Page:1144-1153
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Desikan S. L. N.¹,Srinivasan K.¹

Affiliation:

1. Vikram Sarabhai Space Centre, Thiruvananthapuram 695 022, India

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.A34088

Reference10 articles.

1. SuzukiK.AbeT. “Transonic, Supersonic and Hypersonic Wind Tunnel Tests on Aerodynamic Characteristics on Re-Entry Body with Blunted Cone Configuration,” Rept. 658, Inst. of Space and Astronautical Science, Tokyo, Japan, March 1995, https://repository.exst.jaxa.jp/dspace/handle/a-is/6614 [retrieved 2018].

2. AugensteinB. W.HarrisE. D. “The National Aerospace Plane (NASP): Development Issues for the Follow-On Vehicle: Executive Summary,” Rept. R3878/1-AF, RAND Corp., Santa Monica, CA, 1993, https://www.rand.org/pubs/reports/R3878z1.html [retrieved 2018].

3. From Scramjet to the National Aero-Space Plane (1964–1986);Hallion R. P.,1987

4. JenkinsD. R., Space Shuttle: The History of the National Transportation System, 3rd ed., Dennis r. Jenkins, May 2001, p. 108.

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