Concepts behind the UK HOTLiP maneuvering projectile program
Author:
Affiliation:
1. DERA, Fort Halstead, Sevenoaks, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-4317
Reference19 articles.
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3. JonesJG,MooreKC,PikeJ,RoePL,AMethod for DesigningLifting Configurations for High Supersonic speeds, UsingAxisymmetricFlowFields. Ingenieur-Archiv, Vol 37, pp 56-72(1968)
4. KimBS,RasmussenML, JischkeMC, Optimisation ofWaverider Configurations Generated from Axisymmetric ConicalFlows. AIAA82-1299 (1982)
5. BowcuttGB,AndersonJD, CapriottiD, Viscous Optimised Hypersonic Waveriders. AIAA87-0272 (1987)
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1. Mechanical Actuators for Guidance of a Supersonic Projectile;Journal of Spacecraft and Rockets;2008-07
2. Mechanical Actuators for Guidance of a Supersonic Projectile;23rd AIAA Applied Aerodynamics Conference;2005-06-06
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