Warm gas thruster system with control valve that has a soft seal

1. A thruster system comprising:

a tank for holding liquid propellant;

a catalyst bed connected with the tank and operable to decompose the liquid propellant and generate a gas;

a plenum connected with the catalyst bed for receiving the gas;

a heat exchanger connected with the plenum, the heat exchanger including a phase change material configured to remove heat from the gas into ambient surroundings of the heat exchanger to cool the gas to a temperature below a threshold temperature and thereby generate a cooled gas;

at least one thruster connected with the heat exchanger to receive the cooled gas;

at least one control valve between the heat exchanger and the at least one thruster controlling flow of the cooled gas to the thruster, the at least one control valve including a soft material seal; and

wherein the threshold temperature corresponds to a maximum use temperature of the soft material seal.

2. The system as recited in claim 1 , wherein the soft material is AF-E-411.

3. The system as recited in claim 1 , wherein the phase change material heat includes indium.

4. A vehicle comprising:

a tank for holding liquid propellant;

a catalyst bed connected with the tank and operable to decompose the liquid propellant and generate a gas;

a plenum connected with the catalyst bed for receiving the gas;

a heat exchanger connected with the plenum, the heat exchanger including a phase change material configured to remove heat from the gas into ambient surroundings of the heat exchanger to cool the gas to a temperature below a threshold temperature and thereby generate a cooled gas;

at least one first thruster connected with the heat exchanger to receive the cooled gas;

at least one second thruster connected with the tank to receive the liquid propellant, wherein each at least one first thruster has an first associated impulse bit, each at least one second thruster has a second associated impulse bit, and the first impulse bit is less than the second impulse bit;

at least one control valve between the heat exchanger and the at least one thruster controlling flow of the cooled gas to the thruster, the at least one control valve including a soft material valve seal; and

wherein the threshold temperature corresponds to a maximum use temperature of the soft material seal.

5. The vehicle as recited in claim 4 , wherein the first associated impulse bit is less than 100 μlbf-sec.

6. The vehicle as recited in claim 4 , wherein the soft material valve seal is AF-E-411.

7. The vehicle as recited in claim 4 , wherein the phase change material heat includes indium.

8. A method comprising:

providing a liquid propellant from a tank to a catalyst bed connected with the tank, the catalyst bed generating a gas by decomposing the liquid propellant;

charging a plenum with the gas;

providing a flow of the gas from the plenum to a heat exchanger connected with the plenum, the heat exchanger including a phase change material removing heat from the gas into ambient surroundings of the heat exchanger to cool the gas to a temperature below a threshold temperature and thereby generating a cooled gas;

providing a flow of the cooled gas from the heat exchanger to at least one thruster connected with the heat exchanger; and

using at least one control valve between the heat exchanger and the at least one thruster to control flow of the cooled gas to the thruster, the at least one valve has a soft material valve seal and the threshold temperature corresponds to a maximum use temperature of the soft material valve seal.

9. The method as recited in claim 8 , wherein the soft material valve seal is AF-E-411.

10. The method as recited in claim 8 , wherein the phase change material heat includes indium.