TECHNIQUES FOR COMPUTING LAUNCHER SETTINGS FOR UNGUIDED ROCKETS,
Abstract
Three techniques for computing the launcher angles required for an unguided rocket to obtain a desired theoretical impact are discussed. These methods take into consideration the fact that the rocket will deviate from its nominal course because of the wind it encounters. One method, a field technique, utilizes the wind weighting principle. The other two utilize an iterative technique on a computer for determining launcher settings. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1966
- Accession Number
- AD0642856
Entities
People
- Bernard F. Engebos
- Louis D. Duncan
Organizations
- Atmospheric Sciences Laboratory