PROPAGATION OF STRONG ELECTROMAGNETIC WAVES IN WEAKLY IONIZED ROCKET EXHAUSTS
Abstract
New calculations are performed to ascertain more fully the proposal of tran mitting powerful sacrificial waves from a rocket through the exhaust and thus diminish the attenuation of weaker signals used for communication. Numerical solution of a nonlinear boundary value problem allows the presentation of results in nondimensional form and a comparison with earlier calculations. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1961
- Accession Number
- AD0266392
Entities
People
- Raul R. Hunziker