Design and performance of a parachute recovery system to recover 155-mm- and 8-inch-diameter artillery shells
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, NM
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-2444
Reference5 articles.
1. 'pepper, W. 9. and Fellerhoff, R . D. "Parachute System to Recover Spinning (250 RPS) 155-mm Shell Subjected t o 20,000 G,s Launch ConditionM, SC-R-68-1806, September 1968.
2. Application of Kevlar to parachute system design
3. 'Summary of Sandia Corporation Field Test Facilities, SM-FTFACS-0, April 1967.
4. ' e i s ,G. E."Peak Pressure, Acceleration and Muzzle Velocity Predictions for the 8-inch Howitzer a t the Tonopah Test Range Using Heated Chargesu, zAND81-2266, November 1981.
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1. Modeling of parachute suspension line wrap;16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2001-05-21
2. The development of a ram air decelerator for the recovery of artillery shells;11th Aerodynamic Decelerator Systems Technology Conference;1991-04-09
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