Spacecraft landing and recovery inflation system

1. An inflation system comprising:

a compressed gas source;

an isolation valve located fluidly downstream of said compressed gas source and fluidly coupled with said compressed gas source;

a manifold located fluidly downstream from said isolation valve and fluidly coupled with said isolation valve;

a plurality of command valves located fluidly downstream from said manifold and fluidly coupled with said manifold; and

a bleed orifice fluidly coupled with said manifold between said isolation valve and said plurality of command valves, wherein said bleed orifice automatically equalizes pressure in said manifold between said isolation valve and said plurality of command valves prior to pressurization of said manifold with compressed gas from said compressed gas source.

2. The inflation system of claim 1 further comprising a command processor in communication with the isolation valve and the plurality of command valves,

wherein said command processor generates inflation initiation command signals in response to an initiation signal;

wherein said command processor generates inflation cessation command signals in response to first pressure signals; and

wherein said command processor generates vent command signals in response to second pressure signals.

3. The inflation system of claim 2 further comprising a plurality of pressure sensors, each pressure sensor of said plurality of pressure sensors being located fluidly downstream from an associated command valve of said plurality of command valves, wherein said plurality of pressure sensors are in communication with said command processor.

4. The inflation system of claim 3 wherein said plurality of command valves are configured to open and allow said compressed gas from said compressed gas source to pass therethrough in response to said inflation initiation command signals.

5. The inflation system of claim 4 wherein said plurality of command valves are configured to close in response to said inflation cessation command signals.

6. The inflation system of claim 3 wherein said plurality of pressure sensors generate said first pressure signals when a first predefined target pressure is detected downstream of said plurality of command valves.

7. The inflation system of claim 6 wherein said plurality of pressure sensors generate said second pressure signals when a second predefined target pressure is detected downstream of said plurality of command valves.

8. The inflation system of claim 3 further comprising at least one redundancy configured to accommodate a failure mode of one or more of said command processor, said plurality of command valves and said plurality of pressure sensors.

9. The inflation system of claim 2 further comprising an airbag assembly located fluidly downstream from said plurality of command valves and fluidly coupled with said plurality of command valves.

10. The inflation system of claim 9 wherein said airbag assembly comprises:

an outer airbag fluidly coupled with one command valve of said plurality of command valves to receive a first portion of said compressed gas; and

an inner airbag positioned within said outer airbag and fluidly coupled with another command valve of said plurality of command valves to receive a second portion of said compressed gas.

11. The inflation system of claim 10 wherein said inner airbag is fluidly coupled with said outer airbag.

12. The inflation system of claim 10 wherein said airbag assembly further comprises a venting mechanism operably coupled to said outer airbag and communicatively coupled to said command processor, and wherein said venting mechanism is configured to vent said first portion of said compressed gas from said outer airbag in response to said vent command signal.

13. A spacecraft comprising:

a space capsule; and

the inflation system of claim 1 associated with said space capsule.

14. The spacecraft of claim 13 further comprising an airbag assembly located fluidly downstream from said plurality of command valves and fluidly coupled with said plurality of command valves.

15. The spacecraft of claim 14 wherein said airbag assembly comprises:

an outer airbag fluidly coupled with one command valve of said plurality of command valves to receive a first portion of said compressed gas; and

an inner airbag positioned within said outer airbag and fluidly coupled with another command valve of said plurality of command valves to receive a second portion of said compressed gas.

16. The spacecraft of claim 13 further comprising a heat shield connected to said space capsule.

17. The spacecraft of claim 13 further comprising a parachute connected to said space capsule.

18. An inflation method comprising:

automatically equalizing pressure in a manifold, located between and fluidly coupled with an isolation valve and a plurality of command valves, using a bleed orifice fluidly coupled with said manifold between said isolation valve and said plurality of command valves;

generating, by a command processor, a first inflation initiation command signal;

actuating, by said command processor, said isolation valve, fluidly coupled to a compressed gas source, in response to said first inflation initiation command signal; and

pressurizing said manifold, located fluidly downstream from and fluidly coupled to said isolation valve, with said compressed gas.

19. The inflation method of claim 18 , further comprising:

generating, by said command processor, a second inflation initiation command signal following pressurization of said manifold;

actuating, by said command processor, said plurality of command valves, located fluidly downstream from and fluidly coupled to said manifold, to open said plurality of command valves and allow said compressed gas to pass therethrough in response to said second inflation initiation command signal;

measuring, by a plurality of pressure sensors, pressure downstream of said plurality of command valves;

generating, by each one of said plurality of pressure sensors, first pressure signals when a first predefined target pressure is detected downstream of said plurality of command valves;

generating, by said command processor, inflation cessation command signals in response to said first pressure signals; and

actuating, by said command processor, said plurality of command valves to close in response to said inflation cessation command signals.

20. The inflation method of claim 19 further fluidly coupling an airbag assembly with said plurality of command valves.

21. The inflation method of claim 19 further comprising:

generating, by each one of said plurality of pressure sensors, second pressure signals when a second predefined target pressure is detected downstream of said plurality of command valves, said second predefined target pressure being greater than said first predefined target pressure; and

generating, by said command processor, vent command signals in response to said second pressure signals.