Some Effects of Roll Rate on the Longitudinal Stability Characteristics of the Hughes Falcon Missile, ''C'' Configuration, for a Mach Number Range of 1.1 to 1.8 as Determined From Flight Test (Listing Multiple Pages).

Pages

This report has 31 pages. Select a thumbnail to view a larger version.

Sequence Number: 1 1
Sequence Number: 2 2
Sequence Number: 3 3
Sequence Number: 4 4
Sequence Number: 5 5
Sequence Number: 6 6
Sequence Number: 7 7
Sequence Number: 8 8
Sequence Number: 9 9
Sequence Number: 10 10
Sequence Number: 11 11
Sequence Number: 12 12
Sequence Number: 13 13
Sequence Number: 14 14
Sequence Number: 15 15
Sequence Number: 16 16
Sequence Number: 17 17
Sequence Number: 18 18
Sequence Number: 19 19
Sequence Number: 20 20
Sequence Number: 25 25
Sequence Number: 26 26
Sequence Number: 27 27
Sequence Number: 28 28
Sequence Number: 29 29
Sequence Number: 30 30
Sequence Number: 31 31
Back to Top of Screen