An analysis of the vertical launch phase of a missile concept
Author:
Affiliation:
1. U.S. Navy, Naval Surface Weapons Center, Dahlgren, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-569
Reference12 articles.
1. of Tactical Weapons to Mach Number 3 and Angle of Attack 15' Part 11 - Computer Program and Usage, Dahlgren, Virginia, March 1971.
2. Missile Boost Acceleration w 1600.
3. 25-20 2 -40 8, = 90 deg sv,= 15deg ta= 0.25 see OCUM = 250 deglsec
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