Monopropellant Thrusters


Moog offers a wide range of monopropellant thrusters suited for spacecraft and flight vehicle attitude control applications. These hydrazine thrusters have a long and successful heritage. Range of applications include; earth observation and communication, space exploration, and missile defense. 

 

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101-102-1-Monopropellant-Thrusters-grey-bckgrd-700x400.psd
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Product LineMONARC 1MONARC 5MONARC 22-6MONARC 22-12LT+HTMONARC 90LTMONARC 90HT MONARC 445
Steady State Thrust0.20 lbf (1N) @280 psia1.4 lbf (5.0 N) @350 psia5 lbf (22N) @250 psia

5 lbf (22N) @242 psia

6.2 lbf (22N) @ 250 psia

21 lbf (93 N) @ 235 psia25 lbf (111 N) @ 225 psia100 lbf (445N) @ 260 psia
Feed Pressure70 – 400 psia (4.8 – 27.6 bar)80 – 420 psia (5.5 – 29.0 bar)70 – 400 psia (4.8 – 27.6 bar)70 – 400 psia (4.8 – 27.6 bar)80 – 400 psia (5.5 – 27.6 bar)80 – 370 psia (5.5 -25.5 bar)70 – 400 psia (4.8-27.6 bar)
Nozzle Expansion57:1135:160:140:140:150:150:1
Valve Power18 watts18 watts30 watts30 watts72 watts 72 watts58 watts
Mass0.83 lbm (0.38 kg) 1.08 lbm (0.49 kg)1.58 lbm (0.72 kg)1.51 lbm (0.69 kg)2.47 lbm (1.12 kg)2.47 lbm (1.12 kg)3.5 lbm (1.6 kg)
Engine Length/Exit Diam5.2 in (13.3 cm) / .2 in (0.5 cm)9.4 in (41.8 cm) /1 in (2.5 cm)8 in (20.3 cm) / 1.5 in (3.8 cm)9 in (22.9 cm) / 1.2 in (5.3 cm)12 in (30 cm) / 3.3 in (8.4 cm)12 in (30 cm) / 3.3 in (8.4 cm)16 in (41 cm) / 5.8 in (14.8 cm)
Nominal Specific Impulse235 sec230 sec228 sec

227 sec (LT)

232 sec(HT)

232 sec232 sec235 sec
Heritage HighlightsP-50, SOLRAD X, MSD, IUE, ISRO APPLE, SUERS, SERVIS-1 Galileo, Sentinel, EMMP-50, SEASTAR, DSCS III, ICO, TRIANA, SMAP, M2020, Jason CS, MMS, EarthCare,  LCROSS, WorldviewATS-3, Skynet, CTS, MSD, BSE, IUE, ETS, SEASAT, CP-9, NTSIII, CS-2, NPP, MPS, LCROSS, JPSSIntelsat IV, COBE, TOPEX, GLAST, PACE, MetOp/MPS, ExoMars, SWOT, GOES, LandSat-8P-50, IUS, ASAT, CHANDRA, RCS, TRS, MPS, ARAV-C, SLS EUS REMGRO, MMS