Spacecraft & Satellite Propellant Tanks

3 Spacecraft & Satellite Propellant Tanks from MT Aerospace meet your specification.
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  • Propellant: Hydrazine
  • 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

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