The Nammo Space Non-Return Valve is compatible with all standard propellants.
The Non Return Valve (NRV) is used to prevent the back flow and mixture of bi-propellant fuels in spacecraft propulsion systems. Chemical propulsion systems need to show the flow of vapours from the propellant tanks to the helium pressurization system and between fuel and oxidiser tanks in a bi-propellant system.
During normal operation of the pressurisation system the valve opens at a predetermined cracking pressure to allow gaseous Helium (GHe) flow to pressurise the respective propellant tanks. When the pressure differential across the valve in the normal flow direction reduces to a predetermined value the valve closes by the action of a preloaded spring thus preventing the reverse flow of gas or vapour when the pressure increases in the reverse flow direction.
Performance Characteristics
Operating Media
GN2, GHe, NTO, MMH, N2H4
Maximum Operating Pressure
36 bar
Proof Pressure
72 bar
Burst Pressure
144 bar
Operating Temperatures
-50°C to +50°C
Flow Rate
up to 5g/s
Pressure Drop
<0.15mbar for 0.24g/s GHe at 18 bar inlet
Internal Leakage
<1 x 10-4 scc/s GHe at 120 bar
with 10bar reverse pressure applied
External Leakage
<1 x 10-6 scc/s GHe at 120 bar
Cycle Life
>200,000 cycles
Filter Rating
15 µm absolute
Wetted Materials
Ti Alloy, Stainless Steel, PTFE
Hardware Mass
<90 gram
Envelope
57 mm diameter x 126 mm length
including stub tubes
Fluidic Interface
1/4” or 3/8” tube stub (weldable)
The interfaces can be customised based on the customer needs.