Evaluation of Airbag Decelerator by Drop Tests.
Abstract
The document describes tests of an airbag decelerator varying the number, location, and size of its orifices and using different thicknesses of diaphragm material covering its orifices to determine the most favorable combination to minimize landing shock (deceleration) of cargo dropped by parachute. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 25, 1953
- Accession Number
- AD0857024
Entities
People
- M. C. Madaffer
Organizations
- Wright Laboratory