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Spacecraft & Satellite Propellant Tanks from Manufacturers in Germany

27 Spacecraft & Satellite Propellant Tanks from 2 Manufacturers meet your specification.
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27 Spacecraft & Satellite Propellant Tanks from 2 Manufacturers
27 Products from 2 Manufacturers
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DIAPHRAGM PROPELLANT TANK DT180 Image
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Orbital Propulsion Centre - DIAPHRAGM PROPELLANT TANK DT180

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:Propellant Tank

Product Specs

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
more info
PTD-177 Image
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MT Aerospace - PTD-177

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
Hydrazine
Operating Pressure:
24 Bar
Propellant Volume:
135 L
Total Volume:
177 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
48 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
15.5 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), EPDM (Diaphragm)
Mounting Interface:
Equatorial Trunnions
Operating Temperature:
0 to 50 Degree C
Space Heritage:
Yes
more info
PTD-222 Image
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MT Aerospace - PTD-222

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:222 L Monopropellant Diaphragm Tank for Spacecrafts

Product Specs

Propellant:
Hydrazine
Operating Pressure:
24.5 Bar
Propellant Volume:
164 to 184 L
Total Volume:
221 to 222.8 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
49 Bar
Proof Pressure:
36.8 Bar
Tank Dry Mass:
17.08 ± 0.2 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), EPDM (Diaphragm)
Mounting Interface:
Polar Mounting
Operating Temperature:
4 to 50 Degree C
Space Heritage:
Yes
more info
PTD-96 Image
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MT Aerospace - PTD-96

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:96L Monopropellant Diaphragm Tank for Spacecrafts

Product Specs

Propellant:
Hydrazine
Operating Pressure:
24 Bar
Propellant Volume:
55 / 68 / 71 L
Total Volume:
96 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
48 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
8.2
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), EPDM (Diaphragm)
Mounting Interface:
Equatorial Mounting Tabs
Operating Temperature:
0 to 50 Degree C
Space Heritage:
Yes
more info
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EPDM - BLADDER TANK BT 01/0 Image
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Orbital Propulsion Centre - EPDM - BLADDER TANK BT 01/0

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:58 L Propellant Tank for Spacecrafts

Product Specs

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
more info
Eurostar Family PTP Image
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MT Aerospace - Eurostar Family PTP

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
MMH, N2O4
Operating Pressure:
20 Bar
Total Volume:
165 L
Pressurant:
Helium
Burst Pressure:
30 Bar
Proof Pressure:
26.2 Bar
Tank Dry Mass:
10.8 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Ti-6Al-4V (PMD)
Mounting Interface:
Polar Mounting
Operating Temperature:
0 to 50 Degree C
Space Heritage:
Yes
more info
T11-0 Image
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Orbital Propulsion Centre - T11-0

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:218 L Propellant Tank for Spin Stabilized Spacecraft

Product Specs

Propellant:
MON, MMH
Operating Pressure:
22 Bar
Total Volume:
218 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
33 Bar
Proof Pressure:
27.5 Bar
Tank Dry Mass:
11 Kg
Tank Material:
Pressure Vessel : Ti6AI4V STA (3.7164.7), Suspension/Ports : Ti6AI4V (3.7164.1)
Mounting Interface:
3 Suspension Tabs for Equatorial Load Introduction
Space Heritage:
Yes
more info
S-XTA-60 Image
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MT Aerospace - S-XTA-60

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
Xenon
Operating Pressure:
187 Bar
Total Volume:
60 L
Burst Pressure:
280.5 Bar
Proof Pressure:
233.8 Bar
Tank Dry Mass:
11.7 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Epoxy-based CFRP / T800 (Overwrapped)
Mounting Interface:
Polar Mounting
Operating Temperature:
0 to 65 Degree C
Space Heritage:
Yes
more info
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SURFACE TENSION PROPELLANT TANK OST 21/0 Image
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Orbital Propulsion Centre - SURFACE TENSION PROPELLANT TANK OST 21/0

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:235 L Propellant Tank for Spacecrafts

Product Specs

Propellant:
MON, MMH
Operating Pressure:
22 Bar
Total Volume:
235 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
44 Bar
Proof Pressure:
33 Bar
Tank Dry Mass:
16 Kg
Tank Material:
Pressure Vessel : Ti6AI4V STA (3.7164.7), Suspension/Ports : Ti6AI4V (3.7164.1), PDM : Ti99.4 (3.7034.1) and Ti6AI4V (3.7164.1), Screens : 304L (1.430...
Mounting Interface:
12 Suspension Tabs with floating nuts M6 x 1
Space Heritage:
Yes
more info
PVG Family 40–75 L Image
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MT Aerospace - PVG Family 40–75 L

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
Helium, Nitrogen
Operating Pressure:
310 Bar
Total Volume:
40 to 75 L
Burst Pressure:
465 Bar
Proof Pressure:
387.5 Bar
Tank Dry Mass:
8.5 to 14.4 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Epoxy-based CFRP / T800 (Overwrap)
Mounting Interface:
Polar Mounting
Operating Temperature:
-30 to 60 Degree C
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

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:Propellant Tank

Product Specs

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
more info
PVG Family 80-120 Image
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MT Aerospace - PVG Family 80-120

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
Helium, Nitrogen
Operating Pressure:
310 Bar
Total Volume:
80 to 120 L
Burst Pressure:
465 Bar
Proof Pressure:
387.5 Bar
Tank Dry Mass:
23.5 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Epoxy-based CFRP / T800 (Overwrap)
Mounting Interface:
Polar Mounting
Operating Temperature:
-30 to 60 Degree C
more info
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SURFACE TENSION TANK OST 31/0 Image
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Orbital Propulsion Centre - SURFACE TENSION TANK OST 31/0

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:104-177 L Propellant Tank for Spacecrafts

Product Specs

Propellant:
Hydrazine
Operating Pressure:
24.60 Bar
Propellant Volume:
78 Litres
Total Volume:
104 to 177 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
49.20
Proof Pressure:
36.90
Tank Dry Mass:
6.85
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
more info
XS-XTA / 1 – 7l Family Image
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MT Aerospace - XS-XTA / 1 – 7l Family

Spacecraft & Satellite Propellant Tank from MT Aerospace
Description:Propellant Tank

Product Specs

Propellant:
Xenon
Total Volume:
1 to 7 L
Tank Dry Mass:
3.5 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube)
Mounting Interface:
Polar Mounting
Operating Temperature:
0 to 55 Degree C
more info
1309 to 1450 Litre Bipropellant Tank. Model OST 26/X Image
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Orbital Propulsion Centre - 1309 to 1450 Litre Bipropellant Tank. Model OST 26/X

Spacecraft & Satellite Propellant Tank from Orbital Propulsion Centre
Description:Bipropellant Tank for Spacecraft Propulsion Systems

Product Specs

Propellant:
MON, MMH
Operating Pressure:
19.5 Bar
Total Volume:
1309 to 1450 L
Pressurant:
Helium, Nitrogen
Burst Pressure:
29.25 Bar
Proof Pressure:
24.375 Bar
Tank Dry Mass:
57 to 61 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:
24 suspension tabs with floating nuts M10 x 1.25
more info
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