Customed-contoured radiant heater system for the YF-12 forebody. 1971 (NASA photo) Several ovens with programmable control are available in the FLL for thermal exposure of coupons and panels, up to 4 ft 3 in., to a maximum of 2000°F. There are six non cycling-type ovens, which are manually set to maintain temperature. The maximum temperatures for these ovens range from 650°F to 1300°F.
Two microprocessor-controlled ovens, with interior dimensions of approximately 2 ft. by 2 ft. by 2 ft. are also available for conducting strain-gage measurement errors to 2000°F. Radiant, conduction, and convection heaters are used in conjunction with the universal testing machines for combined loading and heating of coupons and panels.
A programmable vacuum/inert atmosphere furnace can be used for testing to 2000°F. The furnace operates with argon, helium, or nitrogen atmospheres as well as in a vacuum. The furnace can control temperature during heating and cooling. Temperature rise rates as high as 5°F per second may be achieved. The hot zone for the test article measures 3 ft. by 3 ft. by 3 ft.
Thermal testing of aircraft and structural components often requires using large frameworks to support banks of radiant heaters, which are custom-contoured to the vehicle or component shape and are erected around the test article. The heaters are constructed of reflectors upon which banks of quartz lamps are mounted. Each bank, or zone of lamps, is wired into a digital, adaptive, closed-loop control system.
2000 degree Farenheit vacuum and inert atmosphere furnace. 1993 (NASA photo) The temperature of each zone is forced to follow a desired time history, based on feedback from a control thermocouple located on the specimen within that zone. As many as 510 zones can be controlled to distribute up to 20 MW of available power. Maximum temperatures of 2500°F, temperature rise rates of 150°F per second, and heating rates of 100 Btu/ft2 per second have been achieved using this system. Actual maximum test temperature limitations are a function of each test setup.
Liquid nitrogen is used when cooling is required to simulate cryogenic fuel or initial conditions of a high-altitude launch. Liquid nitrogen storage tanks of 1,000 and 4,000 gallon capacity are available at the FLL. Additional cooling gas is provided by two vaporizing systems which convert liquid nitrogen into a gas. These units have a capacity of 2,500 gallons and produce 740 scfm of nitrogen gas each. The outlet gas temperature may be varied from -200°F to +80°F.