Upload
others
View
9
Download
0
Embed Size (px)
Citation preview
Propulsion Valves
Testing Capabilities
• Class 10,000 Cleanroom
• Class 100 Flow Bench
• NVR & Particle Counting for Level 100/A
• Thermal Testing
• Helium Leak Testing
• Bubble Point Testing (Filter)
• Performance Testing
• Filtered Nitrogen & DI-Water Testing
• Heated DI-Water / Nitrogen Aerated Flush
• Acceptance Verification Testing
Available Features
• Suspended Armature
• Bi-Directional
• Magnetic Latching
• Direct Acting / Pilot Operated
• Position Indication
• Proportional / Throttling
RAM Company specializes in the design and manufacture of custom thruster/propellant control valves for mili-tary and commercial Space applications. From orbit insertion and descent to attitude control systems, RAM’s propulsion valves are currently operating on a wide range of spacecraft platforms. With advancements in fluid and temperature compatibility, as well as a firm commitment to quality and cost re-duction, RAM sets itself apart in the rapidly growing Space industry.
Performance Characteristics
• Operating Pressure: up to 1,800 psia
• Non-Operating Pressure: 4,300 psia
• Operating Temperature: -80° F to 400° F
• Flow Rate: .0009 to 1.6 lbm/sec
• Response Time: less than 5 ms
• Life Cycle: Exceeds 1,000,000 (Dry / Wet)
Propellants and Fluids
• Monomethylhydrazine (MMH)
• Nitrogen Tetroxide (NTO)
• Hydrogen Peroxide
• Liquid Nitrous Oxide and Propane
• Kerosene
• Gaseous Methane, Oxygen, Nitrogen, Helium
• Xenon and Argon
• Green Propellants
435-673-4603 www.ramcompany.com [email protected]—
ISO 9001/AS9100 3172 E. Deseret Drive South, St. George, Utah USA Made in America—
Specializing in Electromechanical Design