Document Details


Title:
Results of Kaman Aircraft Corporation Rotochute Test No. 2 Conducted on October 8-12, 1956.
Author(s):
Pepper, W B [Organization 5141]
Document Type:
REPORT
Publication Date:
1957 Jan 11
Document Pages:
27 p.
Document Number(s):
SC-TM-278-56(51); ALSNL199700000602
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
Description/Abstract:
Preliminary results of tests which covered the effects of solidity, blade mass, blade center-of-gravity location, and spring constant on rotor speed and rotor drag over the low speed range of 0 to 300 feet per second.


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