ANALYSIS OF MISSILE LAUNCHERS. PART O PHASE I (MULTI-DEGREE OF FREEDOM MODELS)

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Abstract:

Continued research is reported on guided missile launchers. The analysis of the straight rail launcher model has been revised to include the effects of a slight initial curvature of the rail and the influence of thrust malalignment. Author

Author(s):
Wempner, G. A. ; Lee, S. K.
Author Organization(s):
ILLINOIS UNIV URBANA
Pagination:
0001

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
*GUIDED MISSILE LAUNCHERS, DIFFERENTIAL EQUATIONS, GUIDED MISSILES, LAUNCHING, MATHEMATICAL ANALYSIS, MOTION, PITCH(MATERIAL), PITCH(MOTION), STABILITY, THRUST, YAW
Report Date:
1961 Aug 01