Computer design code for conical ribbon parachutes

Author:

WAYE D.1

Affiliation:

1. Sandia National Laboratories, Albuquerque, NM

Publisher

American Institute of Aeronautics and Astronautics

Reference3 articles.

1. Table 1 Sample Program Output HORIZONTAL RIBBON TOP LTH RIBBON 1 (VENT) = 1.2906 RIBBON 2 = 1.a442 RIBBON 3 = 2.3977 RIBBON 4 = 2.9512 RIBBON 5 = 3.5047 RIBBON 6 = 4.0583 RIBBON 7 = 4.6118 RIBBON 8 = 5.1653 RIBBON 9 = 5.7188 RIBBON 10 = 6.2724 RIBBON 11 = 6.7798 RIBBON 12 = 7.2872 RIBBON 13 = 7.7946 RIBBON 14 = 8.3020 RIBBON 15 = 8.8093 RIBBON 16 = 9.3167 RIBBON 17 = 9.8241 RIBBON 18 = 10.3315 RIBBON 19 = 10.8389 RIBBON 20 = 11.3463 RIBBON 21 (SKIRT)= 11 .a537

2. BOT LTH 1.6597 2.2132 2.7667 3.3202 3.a738 4.4273 4.9808 5.5343 6.0879 6.641 4 7.1488 7.6562 8.1636 8.6710 9.1784 9.6858 10.1932 10.7006 11.2080 11.7154 12.2227 WIDTH 1 .oooo 1.oooo 1 .oooo 1 .oooo 1 .oooo 1 .a000 1 .oooo 1.0000 1 .oooo 1 .oooo 1 .oooo 1 .oooo 1 .oooo 1.oooo 1 .oooo 1.0000 1 .oooo 1 .a000 1 .oooo 1 .0000 1 .oooo SPACE .5000 .5000 .5000 .5000 .5000 .5000 .5000 .5000 .5000 .3750 .3750 .3750 .3750 .3750 .3750 .3750 .3750 .3750 .3750 .3750

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The development of a spreadsheet-aided-engineering design tool for parachutes;14th Aerodynamic Decelerator Systems Technology Conference;1997-06-03

2. Preliminary characterization of parachute wake recontact;Journal of Aircraft;1990-06

3. A preliminary characterization of parachute wake recontact;10th Aerodynamic Decelerator Conference;1989-04-18

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