Z(WS 107A-1)ZFlight Test Working Group Flight Test Report Atlas Missile 35E, 1 December 1961, AMR Range Test Number 5462 Astronautics Test Number P3-501-00-35.
Abstract
The primary purposes of this flight were to obtain data on the location of the re-entry vehicle impact for the statistical determination of the CEP, to determine re-entry vehicle and missile system compatibility, to evaluate the Inertial Guidance System performance, to evaluate the performance of the Acoustica PU System and to determine the open loop performance of the tank fragmentation system. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 08, 1961
- Accession Number
- AD0844824
Entities
Organizations
- General Dynamics