Angular accelerometer
An angular accelerometer designed for integration into gyro-stabilized platforms, providing measurement of apparent acceleration for ballistic and space equipment.
Key figurescomparable across the catalogue
- Mass
- 0.3 kg
- Design life
- 17 years
- Lead time
- 7 months
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Purpose
- Working as part of a gyro-stabilized platform.
- Year of release
- 1986
- Design life
- 17 years
- Lead time
- 7 months
- Flight qualification of the product
- yes
- Brief history of flight qualification
- as part of the LV "Rokot"
- Height
- 85 mm
- Diameter
- 50 mm
- Mass
- 0.3 kg
About
This angular accelerometer is specifically designed to function as an integral part of a gyro-stabilized platform. Its primary purpose is to measure the apparent acceleration experienced by ballistic and space equipment. The product was first released in 1986 and boasts a guaranteed service life of 17 years. It has undergone flight qualification, with a notable heritage as part of the ‘Rokot’ launch vehicle. The estimated production and delivery time for this accelerometer is 7 months. While the page does not specify possibilities for adaptation to customer requirements, its core function is clearly defined for space applications.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.