Corrective Propulsion System 95
Glavkosmos
The AIPD-95 corrective propulsion system is designed for spacecraft orbit correction and maintenance, featuring a pulsed operating mode with a 1 Hz pulse repetition rate.
Key figurescomparable across the catalogue
- Mass
- 20 kg
- Power
- 180 W
- Thrust
- 0.003 N
- Specific impulse
- 0.143 s
- Design life
- 7 years
- Lead time
- 12 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
- The AIPD-95 corrective propulsion system is designed to perform the correction of the orbit, as well as to maintain orbit parameters during the operation of the spacecraft.
- Year of release
- 2009
- Design life
- 7 years
- Lead time
- 12 months
- Flight qualification of the product
- No
- Possibility to adapt the product to customer requirements
- Yes
- Total thrust
- 16.2 kN · s
- Specific impulse of traction
- 1.4·104 m/s
- Engine thrust
- 3.2 mN
- Power consumption cps aipd-95
- 180 W
- Weight cps aipd-95
- 20 kg
- Supply voltage
- 26-34 V
- Guaranteed pulses
- 9·106
About
The AIPD-95 corrective propulsion system is engineered to perform orbit correction and maintain orbit parameters during the operational lifespan of a spacecraft. This system, released in 2009, has a guaranteed service life of 7 years. It consists of a monoblock that integrates an AIPD-95 CPS engine, a BPU-150 device, and a set of mounting parts. The AIPD-95 CPS engine itself comprises a KNE block, a BIR1 block, and a BIR2 block. The system is also equipped with KIA CPS. The operating mode of the AIPD-95 CPS is pulsed, with a pulse repetition rate of 1 Hz. Although flight qualification is not yet achieved, flight operation is planned from 2021. The product can be adapted to customer requirements. The estimated production/delivery time is 12 months.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.