3 Axis Accelerometer (MESA) for Cannonball 2
Abstract
A triaxial accelerometer system was developed for flight on the Cannon Ball 2 satellite (OAR 901). This report provides the necessary operating and diagnostic instructions for this research equipment. Included are operation and calibration instructions, interconnection diagrams, logic diagrams, schematics and assembly drawings.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 15, 1971
- Accession Number
- AD0738657
Entities
People
- Murray A. Meldrum
- William G. Lange
Organizations
- Bell Aircraft Corporation