Nammo Space has responded to the growing requirement for demisable tanks required for small launchers and spacecraft.
The inherent risk of non-demisable Titanium Alloy tanks surviving re-entry and falling to Earth is recognised. Nammo Space has utilised specially developed forging and friction stir welding capabilities at its Raufoss manufacturing facility to create spacecraft propellant tanks in Aluminium Alloy.
Nammo’s metallurgists and chemists have carried out analysis and propellant compatibility testing of high strength Aluminium alloys with hydrazine derivatives, NTO and Hydrogen Peroxide. Using the alloys that pass the selection and mechanical performance criteria, tank shells are forged, machined and assembled with moulded diaphragms and appropriate welding techniques. The tanks are then proven through a complex and intensive inspection and testing regime, before being delivered for propulsion system integration.
Performance Characteristics
Storage Fluids
87.5% H2O2, MON, MMH
Compatibility testing is available for other fluids.
Pressurant
Nitrogen
Helium gas can also be used
Tank Type
Positive Expulsion Device (Diaphragm type)
Useable Propellant Volume
45.5 Litres
Mass
< 13 kg
Maximum Expected Operating Pressure
32 bara
Proof Pressure Factor
1.5
Burst Pressure Factor
> 2
Expulsion Efficiency
> 99%
Blowdown Ratio
2.7
Tank Form
Spherical domes with cylindrical mid-section
Dimensions (at interfaces)
ø490 mm x H 650 mm
Equatorial mounting
External Leakage
1 x 10-6 scc/s
Diaphragm Material
Viton
Tank Structure Material
AA6000 series T6
Structural Interface
Equatorial adapters
Interfaces are customisable, please contact Nammo for further details.