Spacecraft & Satellite Propellant Tanks - Page 2

334 Spacecraft & Satellite Propellant Tanks from 6 Manufacturers meet your specification.
334 Spacecraft & Satellite Propellant Tanks from 6 Manufacturers
334 Products from 6 Manufacturers
Page 2 of 23
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
Description:Propellant Tank for Launch Vehicles

Product Specs

Operating Pressure:
20.7 Bar
Propellant Volume:
157.6 L
Total Volume:
186 L
Tank Dry Mass:
19.1 Kg
more info
Description:Propellant Tank

Product Specs

Propellant:
Hydrazine, IPA, Distilled Water, GN2, GHe
Operating Pressure:
5.5 to 25.4 Bar
Propellant Volume:
30 L
Total Volume:
37.5 L
Pressurant:
GN2, GHe
Burst Pressure:
58.2 Bar
Proof Pressure:
38.1 Bar
Tank Dry Mass:
3.9 Kg
Tank Material:
Ti- 6 Al-4V
Mounting Interface:
Pedestal Mounting
Operating Temperature:
4 to 55 Degree C
Space Heritage:
Yes
more info
Description:30L Satellite Propellant Tank

Product Specs

Propellant:
MMH, MON
Operating Pressure:
24 Bar
Propellant Volume:
30 L
Total Volume:
30 L
Burst Pressure:
96 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
5.7
Tank Material:
Ti-6Al-4V in STA and annealed condition, commercially pure Titanium and SS-304L
Mounting Interface:
18 holes of 5.5 Dia on 214 PCD
Operating Temperature:
5 to 55 Degree C
more info
Advertisement
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
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
Description:Propellant Tank for Launch Vehicles

Product Specs

Operating Pressure:
22.1 Bar
Total Volume:
49.1 L
Tank Dry Mass:
5.6 Kg
more info
Description:7.5 Kg Spacecraft and Satellite Propellant Tank

Product Specs

Propellant:
Hydrazine, IPA, Distilled Water, GN2, GHe
Operating Pressure:
5.5 to 24.6 Bar
Propellant Volume:
75 L
Total Volume:
102.5 L
Pressurant:
GN2, GHe
Burst Pressure:
49.2 Bar
Proof Pressure:
36.9 Bar
Tank Dry Mass:
7.5 Kg
Tank Material:
Ti- 6 Al-4V
Mounting Interface:
Polar Mounting
Operating Temperature:
4 to 60 Degree C
Space Heritage:
Yes
more info
Advertisement
Description:35L Propellant Tank

Product Specs

Propellant:
MMH, MON
Operating Pressure:
24 Bar
Propellant Volume:
35 L
Total Volume:
35 L
Burst Pressure:
96 Bar
Proof Pressure:
36 Bar
Tank Dry Mass:
7 Kg
Tank Material:
Ti-6Al-4V in STA and annealed condition, commercially pure Titanium and SS-304L
Mounting Interface:
16 holes of 5.5 Dia on 214 PCD
Operating Temperature:
5 to 55 Degree C
more info
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
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
Description:Propellant Tank for Launch Vehicles

Product Specs

Operating Pressure:
27.3 Bar
Propellant Volume:
12.5 L
Total Volume:
17.7 L
Tank Dry Mass:
2.5 Kg
more info
Advertisement
Description:Propellant Tank

Product Specs

Propellant:
Hydrazine, IPA, Distilled Water, GN2, GHe
Operating Pressure:
5.5 to 27.4 Bar
Propellant Volume:
154 L
Total Volume:
204 L
Pressurant:
GN2, GHe
Burst Pressure:
54.8 Bar
Proof Pressure:
41.1 Bar
Tank Dry Mass:
17.5 Kg
Tank Material:
Ti- 6 Al-4V
Mounting Interface:
Polar Mounting
Operating Temperature:
4 to 50 Degree C
Space Heritage:
Yes
more info
Description:390L Propellant Tank for Satellites

Product Specs

Propellant:
MMH, MON
Operating Pressure:
16.5 Bar
Propellant Volume:
390 L
Total Volume:
390 L
Burst Pressure:
33 Bar
Proof Pressure:
24.75 Bar
Tank Dry Mass:
23 Kg
Tank Material:
Ti-6Al-4V in STA and annealed condition, commercially pure Titanium and SS-304L
Mounting Interface:
18 Nos. of M6x1 floating plate nuts on Dia 877mm
Operating Temperature:
5 to 55 Degree C
more info
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
Advertisement