Corrective Propulsion System UD-AIPD
Moscow Aviation Institute
The UD-AIPD is a corrective propulsion system designed for spacecraft orientation and correction, featuring a monoblock design and operating in a pulsed mode.
Typed specifications7 values
Discloses 3 of 11 fields engineers filter by in this category (category median 3).
- Mass
- 8 kg product page
- Thrust
- 3 mN product page 3 mN
- Supply voltage
- 26–34 V product page
- Power consumption
- 150 W product page
- Design lifetime
- 15 years product page
- Lead time
- 12 months product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier13 lines, in the manufacturer's own wording
- Purpose
- The corrective propulsion system UD-AIPD is intended for use as part of systems for the correction and orientation of spacecraft for various purposes.
- Year of release
- 2007
- Design life
- 15 years
- Lead time
- 12 months
- Flight qualification of the product
- No
- Possibility to adapt the product to customer requirements
- Yes
- Total thrust
- 20 kN · s
- Specific impulse of traction
- 1.35·104 m/s
- Engine thrust
- 3 mN
- Power consumption cps aipd-95
- 150 W
- Weight cps aipd-95
- 8 kg
- Supply voltage
- 26-34 V
- Guaranteed pulses
- 2·107
About
The Corrective Propulsion System UD-AIPD is engineered for integration into spacecraft systems to facilitate correction and orientation maneuvers. Released in 2007, it boasts a guaranteed service life of 15 years. The system is designed with a monoblock structure, incorporating the KNE block, BIR1, BIR2 blocks, and a discharge accelerator channel. It also includes a set of mounting parts for installation. The UD-AIPD operates in a pulse mode with a repetition rate of 4 Hz. While the product is not flight qualified, it offers the possibility of adaptation to meet specific customer requirements. Key specifications include a total thrust of 20 kN·s, a specific impulse of traction of 1.35·10^4 m/s, an engine thrust of 3 mN, power consumption of 150 W, a weight of 8 kg, and a supply voltage range of 26-34 V. It is guaranteed for 2·10^7 pulses.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.