Spacecraft & Satellite Propellant Tanks - MT Aerospace

11 Spacecraft & Satellite Propellant Tanks from MT Aerospace meet your specification.

Spacecraft & Satellite Propellant Tanks from MT Aerospace are listed on SatNow. We have compiled a list of Spacecraft & Satellite Propellant Tanks from the MT Aerospace website/catalog and made their products searchable by specification. Use the filters to narrow down on products based on your requirements. Download datasheets and request quotes for products that you find interesting. Your inquiry will be directed to MT Aerospace and their distributors in your region.

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  • Manufacturers: MT Aerospace
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
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
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 Kg
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
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
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
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
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
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
Propellant:
Xenon
Operating Pressure:
187 Bar
Total Volume:
40 to 120 L
Burst Pressure:
280.5 Bar
Proof Pressure:
233.8 Bar
Tank Dry Mass:
6.3 to 14.8 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Epoxy-based CFRP / T800 (Overwrap)
Mounting Interface:
Polar Mounting
Operating Temperature:
0 to 65 Degree C
more info
Propellant:
Xenon
Operating Pressure:
187 Bar
Total Volume:
600 to 900 L
Burst Pressure:
280.5 Bar
Proof Pressure:
233.8 Bar
Tank Dry Mass:
68 to 85 Kg
Tank Material:
Ti-6Al-4V (Shell), Ti-3Al-2.5V (Tube), Epoxy-based CFRP / T800 (Overwrap)
Mounting Interface:
Equatorial Skirt
Operating Temperature:
0 to 50 Degree C
more info