Results of Kaman Aircraft Corporation Rotochute Test No. 2 Conducted on October 8-12, 1956.
1957 Jan 11
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
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.