TESTS OF AN ARRESTING CABLE POP-UP SYSTEM
Abstract
The aircraft engaging system was installed on a test runway. Engagement tests were conducted with B-47B, F-84G and F -!))A aircraft. Operational engagements were successfully completed on a break-away hook on the F-84G and F-100A, and on a st ndard arresting hook on the B-47B. Engagements were made at velocities of 11 to 165 knots. Successful emergency e gagements were made on the main wheel struts at velocities of 14 to 143 knots. The equipment and procedures for conducting these tests are described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1961
- Accession Number
- AD0266319
Entities
People
- J.a. Zdrazil