RDS - A PC-based aircraft design, sizing, and performance system

Author:

RAYMER DANIEL1

Affiliation:

1. Conceptual Research Corp., Sylmar, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. To c a l c u l a t e d c o s t s i n o t h e r than 1986 d o l l a r s i t i s necessary t o e n t e r an economic escalation ( i n f l a t i o n ) f a c t o r (then-year-dol1ars/l986 dol 1ars) as we11 as t o e n t e r t h e h o u r l y r a t e s f o r engineering,production, etc. i n thenyear d o l l a r s . Only development and procurement costs are estimate.

2. drawn, resized, groundroll, groundroll, M.9 M1.4 M1.8 M1.4 time, T/W w/s Ib Ib ft ft n=5 n=5 n = l n=l S 1.18 44.8 11,647 31,688 546 749 243 376 794 146 30.6 1.18 56 11,324 25,188 659 914 122 341 922 210 29.2 1.18 67.2 11,102 22,060 771 1071 -13 302 1027 261 28 0.98 44.8 11,271 21,232 629 811 137 122 446 11 41.5 0.98 56 10,947 17,302 763 990 16.5 87 573 74 39.0 0.98 67.2 10,725 15,396 896 1168 - 120 48 680 127 37

3. drawn, resized, groundroll, groundroll, M.9 M1.4 M1.8 M1.4 time, T/W w/s Ib

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