Retractable Mast Mechanism
A linear electromechanical mechanism designed for the deployment and fixation of umbrella-type deployable reflectors on spacecraft.
Key figurescomparable across the catalogue
- Mass
- 12 kg
- Largest dimension
- 4,100 mm
- Design life
- 14.5 years
- Lead time
- 6 months
- TRL
- 9
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
- Deployment of the reflector from the transportation to the operational position and its fixation.
- Year of release
- 2005
- Design life
- 10 years
- Lead time
- 6 months
- Mast retraction time
- 30 min
- Generated force, n, not exceeding
- 2500
- Positioning precision
- 0.1 mm
- Operating temperature range
- -40 to +50 °C
- Operational life defined by cycles
- 50
- Active lifetime
- 10 years
- Overall guaranteed lifetime
- 14.5 years
- Overall dimensions
- 252 × 252 × 4100 mm
- Mass
- 12 kg
About
The Retractable Mast Mechanism is a linear electromechanical device specifically engineered for the deployment of umbrella-type deployable reflectors from their stowed transportation position to their operational configuration, followed by their secure fixation. This mechanism was first released in 2005 and boasts a guaranteed service life of 10 years. It offers precise positioning with an accuracy of 0.1 mm and can operate within a temperature range of -40 to +50 °C. The operational life is defined by 50 cycles, and it has an active lifetime of 10 years, with an overall guaranteed lifetime of 14.5 years. The mechanism generates a force not exceeding 2500 N and has a mast retraction time of 30 minutes. Its overall dimensions are 252 x 252 x 4100 mm, and it has a mass of 12 kg. Estimated production and delivery time is 6 months.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.