HARDWARE / PRODUCTUpdated 24 Jul 2026

Green mono-propellant Micro Propulsion System (MiPS)

VACCO Industries
Green mono-propellant Micro Propulsion System (MiPS)

The VACCO Green MiPS is a self-contained 3U mono-propellant propulsion system for CubeSats, featuring four 100 mN thrusters and providing 3,320 N-sec of total impulse.

Typed specifications41 values

Discloses 8 of 11 fields engineers filter by in this category (category median 3).

Propulsion family
chemical
datasheet p.1
Mass
3 kg
max · Dry Mass · datasheet p.1 5 kg max · Wet Mass 95% Fill @ 10°C
Thrust
100 mN
datasheet p.1 100 mN each thruster
Envelope (L×W×H)
8.860 in (225.0 mm) x 4.080 in (103.6 mm) x 5.784 in (146.9 mm)
datasheet p.2
Total impulse
3 320 N·s
total @10°C · datasheet p.1
Propellant
ADN green (LMP-103S/LT)
datasheet p.1 LMP-103S (ADN) configurable: ADN green (LMP-103S/LT)  |  AF-M315E (HAN) configurable: Air Force green (AF-M315E)  |  Air Force green (AF-M315E)
Supply voltage
5 V
nom. · telemetry, 5±0.25 VDC · datasheet p.1 5±0.25 VDC Operating Voltage For Telemetry  |  5 V Operating Voltage For Telemetry; ±0.25 V; as stated: «5±0.25 …  |  9.5–12.6 V Operating Voltage For Heaters & Valves
Power consumption
1 W
health and status monitoring · datasheet p.1 1 W warmup (as printed)  |  1 W Warmup Power  |  1 W max · health and status monitoring (< 1 Watt)  |  10 W max · standby (as printed)  +2
Data interface
RS-422
datasheet p.1
Operating temperature
10–40 °C
datasheet p.1
Thruster technology
monopropellant green (ADN or HAN)
datasheet p.1
Thrusters in the unit
4
datasheet p.1
Volume
3 U
approximately 3U · datasheet p.1
Propellant mass (full load)
2 kg
datasheet p.1 2 kg tank contains 2 kg of propellant
Feed / tank pressure
29.1 bar
GHe MDP · datasheet p.1 29.1 bar GHe MDP (422 psia)  |  5.17 bar Propellant MDP  |  5.17 bar propellant MDP (75 psia)
Power at thrust
15 W
max · 4 thrusters · datasheet p.1
Survival temperature
-34–60 °C
datasheet p.1 -34–60 °C non-operating
Flight heritage
Flight systems currently in production.
datasheet p.1
Satellite class
CubeSat
datasheet p.1
Delta-v
237 m/s
for a 14 kg CubeSat · datasheet p.1
Power processing unit included
yes
datasheet p.1
Dry mass
3 kg
max · datasheet p.1

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 supplier10 lines, in the manufacturer's own wording
Performance density
969 N-sec/L
Volume
approximately 3U
Number of thrusters
four
Thruster thrust
100 mN
Total impulse
3,320 N-sec
Delta-v (for a 14 kg CubeSat)
237 m/s
Propellant capacity
2 kg
Interface
RS-422
Power consumption (health and status monitoring)
< 1 Watt
Configurable for mono-propellants
ADN green (LMP-103S/LT), Air Force green (AF-M315E)

About

The VACCO Green mono-propellant Micro Propulsion System (MiPS) offers a highly reliable, self-contained solution for CubeSat attitude control and main propulsion. This system occupies approximately 3U in volume and is equipped with four 100 mN thrusters. It delivers a total impulse of 3,320 N-sec, enabling a delta-V of 237 m/s for a 14 kg CubeSat. Each thruster operates independently, allowing for both delta-V maneuvers and Attitude Control System (ACS) operations, all managed by an integrated microprocessor controller. The system features an integral titanium fluid control manifold and low-friction, space-grade valves. Its all-welded tank construction can contain 2 kg of propellant. An integrated microcontroller and RS-422 interface facilitate high-level commands from the host spacecraft. The system boasts low power consumption, requiring less than 1 Watt for health and status monitoring. It is easily configurable for various mono-propellants, including ADN green (LMP-103S/LT) and Air Force green (AF-M315E). Flight systems are currently in production.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: cubesat-propulsion.com ↗

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