Ammonia Propulsion
Utilizing the throttling cooling characteristics of liquid ammonia and converting the low-temperature liquid ammonia to a fully gaseous state through heat exchange, the storage tank and evaporator are integrated, allowing for rapid startup. The storage tank and thruster module can be designed with integrated integration to achieve a lightweight propulsion module and high-precision constant thrust output with low power consumption.
Description
| Item | Standard Indicator | Thermal Resistance Indicator |
| Single Thrust | 5~100mN | 5~100mN |
| Number of Thrusts | 1~24 | 1 |
| Single Jet Duration | ≥300s | ≥300s |
| Number of Switches | ≥50,000 times | ≥50,000 times |
| Specific Impulse | ≥110s | ≥150s@100mN |
| Total Impulse | 300~3000Ns (Recommended) | 300~5000Ns (Recommended) |
| Mass | 0.4kg (excluding tank and propellant) | 0.7kg (excluding tank and propellant) |
| Maximum Power Consumption | Single Thruster 1.5W | 40W |
| Operating Temperature | 0~45℃ | 0~45℃ |
| Lifespan | Storage 2 years, in-orbit life | Storage 2 years, in-orbit life superior to |
| 3 years | 3 years | |
| Power Supply | 28/12V | 28/12V |
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E-mail
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