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Supplier: RS Components, Ltd.
Description: 25 â†' 130 W continuously controllable. Piezo ignition. Mains-independent â€" Operation with standard butane lighter gas. Soldering tips temperature up to 580 °C. Anti-static. Approx. 120 min operating time per gas filling Kit Contents = Cleaning sponge, Deflector,
- Equipment Type: Soldering Equipment
- Equipment Type: Gun / Iron / Torch
Supplier: CableOrganizer.com, Inc.
Description: What's special about Duraflex? Prevents damage from UV, gasoline, engine chemicals and salt Resists cuts, abrasion and penetration No damage after 100,000 abrasion cycles 0.09" wall thickness resists snagging Flexible and economical general purpose protection Deflects highShow More
Supplier: Tele-Communication, Inc.
Description: of wee-hour gaming sessions With single-ear cushion, you can flame online enemies and hear the hushed, reverential tributes of envious onlookers Documents and Downloads GameCom X10 Datasheet Fire up your Xbox gaming experience with the Plantronics GameCom X10 headset. Boasting high-qualityShow More
Supplier: Acoustical Solutions, Inc.
Description: . The sculpted surface of the foam panels deflects sound waves allowing the open cell Willtec material to convert sound energy into quiet, kinetic energy. Sonex One acoustic foam is Class 1 Fire Rated.
- Foam Type: Open Cellular
- Form / Shape: Fabricated Shapes / Parts (Molded, Cast)
- Material / Composition: Plastic / Polymer
- Polymer / Chemical System: Specialty / Other
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FIT Rugged Sleeving for Hazardous Applications
, more flexible than spiral wrap or split convoluted tubing, available with an installation tool for fast and easy wrap-around installation. Flame resistant and flame retardant constructions available. • Advanced Performance Expandable Sleeving: 20-mil nylon polyamide monofilament for (read more)
Browse Protective Sleeving Datasheets for Alpha Wire
CLA 5 Fire and Flash Point Tester
The automatic Cleveland Open-Cup (COC) measures and describes the properties of a sample in response to heat and a test flame under controlled conditions. The flash point measures (read more)
Browse Property Testing Equipment Datasheets for Anton Paar
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Journal of Spacecraft and Rockets > Space Shuttle Solid Rocket Motor Plume Pressure and Heat Rate Measurements
The solid rocket booster main flame deflector at NASA Kennedy Space Center Launch Complex 39A was instrumented to measure heat rates, pressures, and temperatures on the final three space shuttle launches.
Space Transportation: A Systems Approach to Analysis and Design > Operations and Support Systems
As vehicle size and duration of liftoff grow, flame deflectors and sound suppression become necessary to dissipaterocket exhaust energy.
Theoretical and experimental evaluation of test cell ''D'' ejector systems (hot flow program)
Because the exhaust gas from a nuclear rocket is highly flammable hydrogen, the open type of flame deflector , which is utilized for testing chemically-fueled rockets, can not be used.
deflector in each flame trench was replaced with two joined and anchored Shuttle flame deflectors .
Study on the Environmental Effects of the Jet on the Launching Tower
The results show that the flame deflector and first layer of the tower suffered serious ablation and impact at the launching process which should be protected specially.
Design to Cope with Fully Developed Fires
The use of self-closing doors, cavity barriers and fire stops, and flame deflectors , that cut off the paths of convective fire spread, is an essential part of the overall fire defense scheme.
Journal of Spacecraft and Rockets > Ignition/duct overpressure induced by Space Shuttle solid rocket motor ignition
0 4 = convection velocity, Eq. (12) = wind velocity = duct coordinates = vertical distance from nozzle exit to flame deflector = vertical distance from flame deflector to duct opening = longitudinal distance of duct ceiling = centerline of wall-jet .
Journal of Spacecraft and Rockets > Computational pollutant environment assessment from propulsion-system testing
The computational grid was generated using the EZSURF code.33 The edge curves of the nozzle exits, aspirator, flame deflector , and multi- zone block edges were generated first.
Journal of Spacecraft and Rockets > Effects of Exhausts from Aluminized Solid Propellants on Launch Facilities
The effects of solid propellant rocket motor (SRM)aluminum content, chamber pressure, nozzle exit diameter, and lift-off acceleration have been evaluated with respect to degradation of protective coatings applied to flame deflectors and umbilical masts.
Journal of Spacecraft and Rockets > Microphone Phased Array to Identify Liftoff Noise Sources in Model-Scale Tests
The presence of the elaborate launch pad is merely to make the plume bend at the location of the flame deflector (Fig. 1).