Centaur Nose Fairing Jettison Test,
Abstract
The object of the test was to evaluate the Centaur Nose Fairing Fuel Vent Duct Seal and disconnect mechanism and to determine the effect of the vent duct disconnect loads on the trajectory of the fairing during jettisoning. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 28, 1961
- Accession Number
- AD0847354
Entities
People
- J. H. Derango
Organizations
- General Dynamics