Monopropellant Thrusters

31 Monopropellant Thrusters from 9 Manufacturers meet your specification.

Monopropellant Thrusters for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

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  • Type: Monopropellant Thruster
SKU:MT-9
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
0.29 to 1.13 N
Thruster Mass:
100 Kg
Specific Impulse:
208 to 215 Sec
more info
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
1.80 to 5.01 N
Thruster Mass:
190 Kg
Specific Impulse:
212 to 225 Sec
more info
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
6.9 to 19.6 N
Thruster Mass:
115 Kg
Specific Impulse:
210 to 226 Sec
more info
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
8.5 to 30 N
Thruster Mass:
140 Kg
Specific Impulse:
212 to 223 Sec
more info
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
23 to 50 N
Thruster Mass:
120 Kg
Specific Impulse:
215 to 225 Sec
more info
Type:
Monopropellant Thruster, Hydrazine Thruster
Thrust:
50 N
Thruster Mass:
107 Kg
Specific Impulse:
225 Sec
more info
Type:
Hydrazine Thruster, Monopropellant Thruster
Thrust:
0.29 to 1.13 N
Specific Impulse:
208 to 215 Sec
Inlet Pressure:
0.55 to 2.76 Mpa
more info
Type:
Hydrazine Thruster, Monopropellant Thruster
Thrust:
1.47 to 5.5 N
Specific Impulse:
206 to 219 Sec
Inlet Pressure:
0.55 to 2.76 Mpa
Space Heritage:
Yes
more info
Type:
Hydrazine Thruster, Monopropellant Thruster
Thrust:
6.9 to 19.6 N
Specific Impulse:
210 to 226 Sec
Inlet Pressure:
0.48 to 2.76 Mpa
Space Heritage:
Yes
more info
Type:
Hydrazine Thruster, Monopropellant Thruster
Thrust:
23 to 50 N
Specific Impulse:
215 to 225 Sec
Inlet Pressure:
0.9 to 2.76 Mpa
Space Heritage:
Yes
more info

What is a Monopropellant Thruster?

A monopropellant thruster is a thruster that uses a single chemical as its propellant. Monopropellants are propellants that consist of chemicals that release energy through exothermic chemical decomposition. This release of energy is usually accomplished with the help of a catalyst. A monopropellant does not require a separate oxidizer.

A Monopropellant thruster generates thrust by allowing liquid propellant to flow through an open valve into a catalytic decomposition chamber. This propellant supply to the thruster happens with one or more than one stage of flow control valves. The thrusters are equipped with an internal catalyst bed heater. A thrust is generated when the control valve is commanded to open causing propellant to be fed to the thrust chamber. When the propellant comes in contact with the catalyst a decomposition reaction takes place within the catalyst bed and the hot decomposition gases are then accelerated through a converging-diverging nozzle.

A monopropellant fuel burns without the need for an oxidizer since the oxidizer is already bound into the molecule. This makes the thruster or engine lighter, less expensive, and more reliable.

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Interface

Space Heritage