LOW COST ACCURATE SENSOR (AB-30). DESIGN STATUS REPORT,
Abstract
A study was made at the Army inertial guidance and control laboratory to determine what design characteristics and parameters must be folewwed to design and manufacture a moderate cost and moderate precision stability sensing gyroscope. Various materialsreere checked and tested for possible use in the manufacture of the gyro rotor, sensing elements, and gyro case. Basic comparisons are tabulated and presented in this report. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 23, 1963
- Accession Number
- AD0416762
Entities
People
- W.e. Grunwald
Organizations
- United States Army Aviation and Missile Command