CAPSTAN DESIGN. (LOW INERTIA TRANSMISSION STUDY).

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Abstract:

A capstan suitable for driving an energy absorber for aircraft recovery systems was designed. Performance analysis of various contours were obtained using a capstan analysis computer program. The design is for a 1-18 inch diameter steel cable and a cable tension ration of 12 to 1. Author

Author(s):
Robinson, Linwood C.
Author Organization(s):
ALL AMERICAN ENGINEERING CO WILMINGTON DEL
Descriptive Note:
Final rept.,
Supplementary Note:
See also AD-708 760.
Pagination:
0036

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AAE-N-585
Contract/Grant Number(s):
N00156-69-C-1897
Project Number(s):
A34-537/200/70F32461405
 Subject Terms
Joint Capability Areas:
JCA_6.1.1_Wired Transmission; JCA_6.1_Information Transport; JCA_6_Net Centric
Communities of Interest:
Air Platforms
Descriptor(s):
*NAVAL SHORE FACILITIES, *AIRCRAFT LANDINGS, *REELS, RUNWAYS, ARRESTING GEAR, ARRESTING GEAR, MECHANICAL CABLES, STEEL, COMPUTER PROGRAMMING
Field(s)/Group(s):
Terminal Flight Facilities, Machinery and Tools
Report Date:
1970 May 25