Three Dimensional Vibration Isolator Analog Computer Analysis.
Abstract
Based on a previous study of a multiaxes isolation system, a mathematical model was made of the isolation system. The resulting equations of motion were nonlinear, ordinary, coupled, and solved on an analog computer. The model strives for realism by including detent forces between the rocket and launcher, rocket exhaust impingement on the frontal surface of the launcher, and mass and inertia changes because of launch. Computer diagrams and lists of data are given by this report. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 18, 1975
- Accession Number
- ADA016878
Entities
People
- E. R. Chubbuck