Cryogenic Special Application Valves


Moog produces a variety of fluid control components used in space launch vehicles as part of their cryogenic fluid control systems. These components handle media including gaseous and cryogenic hydrogen and oxygen, and provide very specific functionality in the cryogenic fluid system. Two of the valves presented below manage tank ullage gas pressure. The third valve works in the propellant feed system, controlling LOx flow to provide a damping capability that reduced the “pogo” effect in the Delta IV launch vehicle. The three valves are pneumatically-operated, using nitrogen or helium to provide actuation pressure. Their pilot-operated designs provide low-weight solutions relative to their flow capacity.

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Key Valve Capabilities Include

  • High performance at temperatures down to -423°F
  • Operating pressures up to 500 psig MEOP
  • Cv = 83-100 gal/minute H2O (vent-relief valve)
  • CdA ≥ 0.3 in2 (Pogo valve)
  • Designs address human rating requirements
101-95-1-Cryogenic-Special-Application-valves-grey-bckgrd-700x400.psd
101-96-1-Cryogenic-Special-Application-valves-grey-bckgrd-700x400.psd
101-97-1-Cryogenic-Special-Application-valves-grey-bckgrd-700x400.psd

 

Valve

Model 50E1389

Vent-Relief Valve

Model 54X164

Continuous Vent Valve

Model 50-918

POGO-Suppression Valve

Media Gaseous Oxygen and Hydrogen Gaseous Hydrogen Liquid and Gaseous Oxygen
Unit Mass 8.5 lbm 4.5 lbm 7.6 lbm
Dimensions (L W H) 5.0” x 5.0” x 11.0” 7.6” x 4.0” x 4.7” 4.3” x 5.4” x 12.0” 
MEOP 500 psig 40 psig Nominal: 300 psig / Surge: 580 psig
Actuation Pressure 500 psig 500 psig 645 psig 
Factors of Safety Proof: 1.5x MEOP; Burst: 2.5x MEOP Proof: 1.5x MEOP; Burst: 2.5x MEOP Proof: 1.5x MEOP; Burst: 2.5x MEOP
Valve Flow Sizing

CV = 83-100 gal/minute H2O

@ 1.0 psid across valve, 60°F 

CdA = 0.2 in2 minimum CdA ≥ 0.3 in2 
Internal Leakage 5 scc/minute GHe

~30 SCIM GHe @ 40 psig and -452°F

(liquid helium)

163 scc/minute GHe ambient/cryogenic
External Leakage 25 scc/minute GHe ~600 SCIM GHe @ -452°F (liquid helium) 5 scc/hour GHe ambient
Actuation Voltage N/A N/A 20 – 34 VDC 
Pull-in / Drop Out Voltage N/A N/A Pull in: ≤ 18 VDC / Drop out: ≥ 2 VDC
Response Time 1 ± 0.5 sec (open or close) 1.5 sec (open or close) 0.100 msec (open or close)
Position Indication N/A Microswitches: one open / one close N/A
Operating Temperature -320°F – 160°F  -423°F – 170°F  -320°F – 160°F 
Filtration  N/A 10 micron nominal, 25 micron absolute  N/A 
Random Vibration 31 Grms

14 Grms – In-Plane Axes

39 Grms – Normal Axis

80 Grms (qual level)
Shock 1000 G 1000 G 1000 G
Cycle Life 500 cycles 400 cycles 1000 cycles 
Materials of Construction Aluminum, CRES, Vespel, PCTFE Aluminium, CRES, PTFE, and PEEK Aluminum, CRES, Vespel, PCTFE

 

Pneumatically Pilot Operated Two Stage Valves

Moog Models 54E131 and 54E132 (Ox and F) are pneumatically pilot operated two stage valves designed for use on a LO2 / Ethanol bipropellant engine. A common design is shared by both propellants but with slightly varied test requirements. This valve contains a small solenoid operated 3-way pneumatic valve as a pilot stage for the main stage liquid valve element. The main stage includes a pneumatic actuator piston that is directly coupled to the propellant valve poppet. The actuator is spring biased to provide a normally closed preloaded condition for the soft seat / poppet interface.

The poppet is inlet pressure balanced to minimize the actuation forces required for operation and the associated size & mass of the entire pilot stage. The following is a list of typical performance characteristics which may be tailored as required for specific application needs.

propulsion

 

Valve

Model 54E131 and 54E132

Pneumatically Pilot Operated Two Stage Valves

Materials of Construction Primarily Stainless Steel
Operating Media GHe, LOx, Ethanol, IPA, DI H2O, GN2
MEOP / Proof / Burst Pressure 390 / 488 / 585 psig (27 / 34 / 40 bar)
Pilot gas pressure 550-650 psi (38 - 45 bar)
Flow Delta P 1.75 lbm/sec (3.86 kg/sec), < 20 psid (<44 bar) H2O
Internal Leakage – main seat <0.2 sccs GN2
Internal Leakage – pilot <0.002 sccs GN2
External Leakage Same as internal leakage
Voltage 20-33 Vdc nominal initial, step down to 10 Vdc nominal for continuous open
Coil Resistance 36 ohms nominal at ambient
Response <50 ms, open or closed
Pull In <0.5 Amp 
Temperature Range -330 to 100°F  (-201 to 38°C) operating
Cycle Life >5000
Mass < 2.0 lbm (<4.4 kg)  Additional weight optimized is possible
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