ASCENT PROBLEMS OF SOUNDING ROCKETS
Abstract
The dynamic stability and wind weighting problems of a spinning sounding rocket are investigated by numerical solution of the six equations of rigid body motion. Transition through the roll resonance regime is discussed, and first-stage trajectory dispersions are compared with those actually measured in flight on five vehicles. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1961
- Accession Number
- AD0287543
Entities
People
- N.l. Crabill
Organizations
- AGARD