DETAIL SPECIFICATION FOR THE Z(XQ-5 HIGH)ZSUPERSONIC DRONE FIRING ERROR INDICATOR SYSTEM.
Abstract
The Firing Error Indicator system shall be designed and fabricated to obtain data indicating the miss distance between the target and the intercepting missile, and to supply these data in suitable form to the telemeter system for transmission to the ground. Miss distance shall be measured in terms of bearing in a plane perpendicular to the target longitudinal axis, and of slant range. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 28, 1958
- Accession Number
- AD0370310
Entities
People
- E. H. Smith
Organizations
- Lockheed Martin