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Hydrazine Propellant Tanks

17 Hydrazine Propellant Tanks from 4 Manufacturers meet your specification.

Hydrazine Propellant Tanks for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

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  • Propellant: Hydrazine
Rolling Diaphragm Tanks Image
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Rolling Metal Diaphragm Propellant Tanks for LEO & GEO Satellites

Hydrazine Propellant Tank from Moog
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SKU:Rolling Diaphragm Tanks
Propellant:
N2O4, MMH, Hydrazine, Amine Fuel
Operating Pressure:
22.4 to 121 Bar
Total Volume:
0.59 to 220 L
Burst Pressure:
39.1 to 181.53 Bar
Proof Pressure:
32.54 to 151.27 Bar
Tank Dry Mass:
0.27 to 27.26 Kg
Tank Material:
Overwrapped Aluminium Alloy, Aluminum Alloy
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177 litre hydrazine surface tension tank. Model OST 31-1 Image
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Orbital Propulsion Centre - 177 litre hydrazine surface tension tank. Model OST 31-1

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
Hydrazine
Operating Pressure:
24 Bar
Propellant Volume:
132 Litres
Total Volume:
177 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
48 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
15 Kg
Tank Material:
Pressure vessel : Ti6AI4V STA (Hemisphere and Rings 3.7164.7), Fluid ports : Ti6AI4V annealed (3, 7164.1), PMD : All titanium
Mounting Interface:
Pole mounting, rigidly fixed at propellant port boss
Space Heritage:
Yes
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331 Litre Hydrazine or Bipropellant Tank. Model OST 25/3 Image
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Orbital Propulsion Centre - 331 Litre Hydrazine or Bipropellant Tank. Model OST 25/3

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
MON, MMH, Hydrazine
Operating Pressure:
19.5 Bar
Total Volume:
331 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
29.25 Bar
Proof Pressure:
24.375 Bar
Tank Dry Mass:
22.7 Kg
Tank Material:
Pressure vessel : Ti6AlV st (3.7164.7), suspension port : Ti6AlV st (3.7164.1), PMD : Ti6Al4V (3.7164.1), Screens : 304L (1.4306)
Mounting Interface:
12 Suspension Tabs with floating nuts M6 x 1
Space Heritage:
Yes
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DIAPHRAGM PROPELLANT TANK DT180 Image
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Orbital Propulsion Centre - DIAPHRAGM PROPELLANT TANK DT180

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
MON, MMH, Hydrazine
Operating Pressure:
35.6 Bar
Total Volume:
180 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
53.4 Bar
Proof Pressure:
44.5 Bar
Tank Dry Mass:
21 Kg
Tank Material:
Ports : Ti6AL4V (3.7164.1), Shell : AA2219-T8, Diaphragm : PTFE basis, C-Ring : Inconel 718
Mounting Interface:
Equatorial flange with 24 fixation bolts M8
Space Heritage:
Yes
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EPDM - BLADDER TANK BT 01/0 Image
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Orbital Propulsion Centre - EPDM - BLADDER TANK BT 01/0

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
Hydrazine
Operating Pressure:
26 Bar
Propellant Volume:
39 Litres
Total Volume:
58 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
52 Bar
Proof Pressure:
39 Bar
Tank Dry Mass:
8.5 Kg
Tank Material:
Pressure Vessel : Ti6AI4V Hemispheres 3.7164.1 (SPF), Gas & Propellant Ports : Ti6AI4V (3.7164.1), Bladder : Ethylene-Propylene-Diene Monomer (EPDM)
Mounting Interface:
5 Fixation Holes ø 8H7
Space Heritage:
Yes
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SURFACE TENSION PROPELLANT TANK OST 33/0 Image
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Orbital Propulsion Centre - SURFACE TENSION PROPELLANT TANK OST 33/0

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
Hydrazine
Operating Pressure:
24.63 Bar
Total Volume:
176.5 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
49.26 Bar
Proof Pressure:
36.95 Bar
Tank Dry Mass:
13.5 Kg
Tank Material:
Pressure Vessel : Ti6Al4V STA (3.7164.7), Trunnions / Port : Ti6Al4V (3.7164.1), PMD : Ti6Al4V (3.7164.1)
Mounting Interface:
4 Suspension Trunnions
Space Heritage:
Yes
more info
SURFACE TENSION PROPELLANT TANK WITH LIQUID COG CONTROL Image
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Orbital Propulsion Centre - SURFACE TENSION PROPELLANT TANK WITH LIQUID COG CONTROL

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
Hydrazine, MON, MMH
Operating Pressure:
18.6 Bar
Total Volume:
198, 282, 331 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
37.2 Bar
Proof Pressure:
27.9 Bar
Tank Dry Mass:
27 Kg
Tank Material:
Pressure Vessel : Ti6Al4V STA (3.7164.7), Suspension/Ports : Ti6Al4V (3.7164.1), PMD : Ti99.4 (3.7034.1) and Ti6Al4V (3.7164.1), Screens: 304L (1.4306...
Mounting Interface:
12 Suspension Tabs with floating nuts M6 x 1
Space Heritage:
Yes
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SURFACE TENSION TANK OST 31/0 Image
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Orbital Propulsion Centre - SURFACE TENSION TANK OST 31/0

Hydrazine Propellant Tank from Orbital Propulsion Centre
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Propellant:
Hydrazine
Operating Pressure:
24.6 Bar
Propellant Volume:
78 Litres
Total Volume:
104 to 177 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
49.2 Bar
Proof Pressure:
36.9 Bar
Tank Dry Mass:
6.85 Kg
Tank Material:
Pressure Vessel : Ti6AI4V STA (Hemispheres 3.7164.7), Gas & Propellant Ports : Ti6AI4V (3.7164.1), Propellant Management Device : All Titanium
Mounting Interface:
Polar Mounting, Rigidly Fixed at Propellant Port Boss Side
Space Heritage:
Yes
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PEPT- 230 Image
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4.5 L Propellant Tank for Satellite Bus

Hydrazine Propellant Tank from RAFAEL
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SKU:PEPT- 230
Propellant:
Hydrazine, IPA, Distilled Water, GN2, GHe
Operating Pressure:
5.5 to 24 Bar
Propellant Volume:
4.5 L
Total Volume:
6 L
Pressurant:
GN2, GHe, Inert Gas
Burst Pressure:
48 Bar (actual rupture >110 bar)
Proof Pressure:
36 Bar
Tank Dry Mass:
1.3 Kg
Tank Material:
Ti- 6 Al-4V
Mounting Interface:
4 lugs at tank
Operating Temperature:
10 to 50 Degree C
Space Heritage:
Yes
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PEPT- 260 Image
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RAFAEL - PEPT- 260

Hydrazine Propellant Tank from RAFAEL
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Propellant:
Hydrazine, IPA, Distilled Water, GN2, GHe
Operating Pressure:
5.5 to 24 Bar
Propellant Volume:
7 L
Total Volume:
9.3 L
Pressurant:
GN2, GHe, Inert Gas
Burst Pressure:
48 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
1.7 Kg
Tank Material:
Ti- 6 Al-4V
Mounting Interface:
4 lugs at tank's equator with ø6.5 mm clearance holes (90° distribution)
Operating Temperature:
10 to 50 Degree C
Space Heritage:
Yes
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