SMALL ROCKET LIFT DEVICE. PHASE II. TESTING OF THE ASSEMBLED UNIT
Abstract
The concept of attaching a rocket propulsion system to a man for transporting him from one place to another was successfully demonstrated. This was done by rigorous static testing of the propulsion system, a manned tethered flight program during which various improvements were incorporated, and finally by a manned free-flight program of various types of maneuvers. Additional quantitative data on stability and control is needed to intelligently establish prototype sp cifications. Hydrogen peroxide, although very successfully utilized, would have a limited tactical use due to its handling characteristics and limitations at low ambient temperatures. A better tactical propellant must be found. The basic concept of distributing the SRLD static weight around the man's body by means of a padded Fiberglas corset proved highly successful. Lifting a man under the arms for a short period of time had no deleterious effects and permits excellent kinesthetic control.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1961
- Accession Number
- AD0267358
Entities
People
- Wendell F. Moore
Organizations
- Bell Aircraft Corporation