Cold Gas Thrusters

101-112-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd



Moog cold gas thruster valves are normally closed direct acting, solenoid actuated devices.

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Overview

Moog produces cold gas thrusters in a variety of thrust ranges to meet mission requirements. Typical thrusts range from 10mN to 4N. Moog cold gas thrusters have flown on Psyche, SAFER, Spitzer Space Telescope, CHAMP, GRACE, and Pluto Fast Flyby.

101-110-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd
101-111-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd
101-112-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd
101-113-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd
101-114-1-Cold-Gas-Thrusters-grey-bckgrd-700x400.psd

 

Parameter 

 

   
PropellantGN2GN2GN2GN2GN, GAr, Xe
MaterialStainless Steel, FluorosiliconeStainless Steel, NylonStainless Steel, AFE411 Stainless Steel, Nylon Stainless Steel, Vespel
Nominal Thrust

10 mN (0.0022 lbf),

16 mN (0.0036 lbf),

40 mN (0.0090 lbf)

@ 1.5 bar (21.75 psia) GN2

120 mN (0.027 lbf)

@ 6.9 bar (100 psia) GN2

120 mN (0.027 lbf)

@ 6.9 bar (100 psia) GN2

3.6 N (0.8 lbf)

@ 15.7 bar (230 psia) GN2

1.3 N @ 90 bar

(1300 psia) Xe inlet,

0.9N @ 90 bar (1300 psia)

GN2 and GAr inlet

Specific Impulse (Nom)> 60 sec> 57 sec65 sec57 sec

21 sec Xe

70 sec GN2

54 sec GAr

MEOP10.0 bar (145 psia)20.7 bar (300 psia)27.6 bar (400 psia)15.7 bar (230 psia)186 bar (2700 psia)
Proof20.0 bar (290 psia)41.4 bar (600 psia)70.0 bar (1015 psia)76.9 bar (1115 psia)279 bar (4050 psia)
Burst40.0 bar (580 psia) 82.7 bar (1200 psia)111.4 bar (1615 psia)155 bar (2250 psia)465 bar (6750 psia)
Leakage - Internal

< 0.1 scch GN2

@ 2.5 bar (36 psid) 

< 0.1 sccm GN2

@ 13.8 bar (200 psid)

< 2.8x10-4 scc/s GHe

< 2.0 sccm GN2

@ 4.1 bar (60 psig)

< 1.0 x 10-4 sccs GHe

@ MEOP

Leakage – External< 1.0x10-5 su/s GHe

< 1.0x10-6 scc/s GHe

@ 27.6 bar (400 psid)

< 1.0x10-6 scc/s GHe

< 1.0 sccm GN2

@ 4.1 bar (60 psig)

<1.0 x 10-6 sccs GHe

@ MEOP

Operating Voltage

22-32 Vdc, 28 Vdc Nominal,

10 Vdc Holding

27-29 Vdc, 28 Vdc Nominal22-34 Vdc, 28 Vdc Nominal27-29 Vdc, 28 Vdc Nominal28 Vdc nominal, 10 Vdc hold
Power10 W open, 1 W holding< 35 W @ 28 Vdc, 20°C

< 10.5 W @ 28 Vdc, 20°C

1.5 W @ 10 Vdc (holding)

30 W @ 28 Vdc, 20°C

10.5 W nominal @

28 Vdc @ 21˚C,

1.3W @ 10 VDc holding voltage

Coil Resistance86 Ohms at 20°C (68°F)26.8 Ohms at 20°C (68°F)75 Ohms at 20°C (68°F)28 Ohms at 20°C (68°F)74.5 Ohms nominal
at 21˚C (68˚F) 
Response – Opening< 2.5 msec

< 3.5 msec @ 28 Vdc,

13.8 bar (200 psia) 

< 5 msec< 4 msec< 10 msec
Response – Closing< 2.5 msec< 3.5 msec @ 28 Vdc,
 13.8 bar (200 psia)
< 3 msec < 4 msec< 10 msec
Life (Cycles)500,000 – 2,000,00020,0001,000,000> 10,000> 100,000
Operating Temperature

-50°C to +60°C

(-58°F to +140°F)

-40°C to +60°C

(-40°F to +140°F)

-25°C to +75°C

(-13°F to +167°F)

-40°C to +60°C

(-40°F to +140°F)

-70°C to +60°C

(-94°F to +140°F) 

Inlet Filtrationnone10 micron Absolute 40 micron Absolute10 micron Absolute 25 micron Absolute
Dimensions

Ø14 mm x 57 mm long

(Ø0.55” x 2.25”)

Ø14 mm x 20.3 mm long

(Ø0.55” x 0.8”)

Ø19.1 mm x 41 mm long

(Ø0.75” x 1.6”)

Ø6.6 mm x 25.4 mm long

(Ø0.26” x 1.0”)

Ø23.8 x 53.1 mm long

(Ø0.94” x 2.1”)

Mass40 grams (0.09 lbm)16 grams (0.035 lbm)70 grams (0.15 lbm)23 grams (0.05 lbm)115 grams max (0.25 lbm) 
HeritageCHAMP and GRACESpitzer Space TelescopeSpitzer Space TelescopeSAFER, Pluto Fast FlybyGEO applications
Model No.

058E143

058E145

058E146

058E142A058E151058-11858E163A