VACCO Thruster Valves
Monopropellant, bipropellant and cold-gas thruster valves for attitude control, reaction control and orbital maneuvering, including the Cold Gas Triad Thruster.
Key figurescomparable across the catalogue
- Thrust
- 2 N
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Valve types
- Monopropellant, bipropellant, cold-gas thruster valves
- Cold gas triad thruster
- 3 x 2 lbf thrusters on a common X/Y/Z manifold block
- Design feature
- Low-friction suspended-armature design
- Flight heritage
- Space Shuttle Manned Maneuvering Unit (MMU) — 4 triad assemblies per unit
- Operating Pressure
- 260 psia
- Proof Pressure
- 630 psia
- Burst Pressure
- 840 psia
- Thrust
- 2.0 lbf
- Internal Leakage
- 3.6 scc/hr GN2
- External Leakage
- 1.08 scc/hr GN2
- Vibration
- 6.28 Grms
- Lifetime
- 150,000 cycles
- Response Time Opening
- 7 msec
- Response Time Closing
- 4 msec
- Flow
- 0.0267 lbm/sec GN2
- Power
- 20 watts
- Operating Voltage
- 12 – 21 VDC
- Pull-In Voltage
- 10 VDC max
- Drop Out Voltage
- 1.0 VDC min
About
VACCO designs and manufactures thruster valves supporting attitude control, reaction control, and orbital maneuvering subsystems (OMS). The line includes monopropellant valves, bipropellant valves, and cold-gas propulsion systems built to meet the space industry’s demand for high cycle life, tight leakage, and quick response, using VACCO’s low-friction suspended-armature design proven on numerous flight programs. The 2-lbf Cold Gas Triad Thruster is an assembly of three identical 2-lbf thrusters mounted on a common manifold block along the X, Y and Z axes. Four of VACCO’s man-rated triad thruster assemblies were used on each Space Shuttle Manned Maneuvering Unit (MMU).
Documentation
- cold_gas_thrusters.pdf PDF source: www.vacco.com ↗
- liquid_propellant_thrusters.pdf PDF source: www.vacco.com ↗
Need the full ICD, test reports or a specific revision? Ask the supplier directly.