Second Of Four Planned J-2X Generator Trials Wraps Up

Engineers at NASA's Marshall Space Flight Center in Huntsville, AL have completed a series of tests on a key component of the J-2X engine which will power the upper stage of the upcoming Ares I rocket.

The test on August 15 was the last of 20 in this series, concluding the second of four planned sets of tests on the J-2X's workhorse gas generator, the driver for the turbopumps which start the engine.

The gas generator test program is designed to demonstrate the component's performance, durability and combustion environment, and to reduce risk in the design, fabrication and operation of flight hardware. The third phase of testing will begin in July 2009. The J-2X's workhorse gas generator is fabricated by Pratt and Whitney Rocketdyne of Canoga Park, CA.

The primary objectives achieved in this series of tests were to regulate ignition timing and address stability issues in the gas chamber. During engine start, a pressurized helium system begins to turn the turbopumps, which draw liquid hydrogen and liquid oxygen propellants into the system. The propellants flow into the generator's combustion chamber, where they are sparked into life by pyrotechnic igniters installed in the side of the main combustion chamber.

Once combustion is initiated, hot gases flow into the turbine. The combustion gas provided by the generator drives the turbomachinery, which delivers high pressure propellants to the main injector during the J-2X burn. This testing allows engineers to address stability issues that can arise during operation of the combustion chamber and will allow engineers to develop a clean design for the J-2X engine.

Beginning in 2015, the Ares I rocket will carry the Orion crew capsule and as many as six astronauts and small payloads to the International Space Station. During the first two-and-a-half minutes of flight, the first stage booster will power the vehicle to an altitude of about 189,000 feet, or 36 miles, at a speed of Mach 4.8. After its propellant is spent, the reusable booster will separate, and the upper stage's J-2X engine will ignite -- powering the Orion to low Earth orbit at an altitude of about 425,328 feet, or roughly 80 miles.

The workhorse gas generator test series is an essential step in development of the J-2X engine. More than 50 tests have been performed on the generator to date. This generator was manufactured to be more durable than the actual generators slated for use in the J-2X engine, allowing it to withstand numerous tests.

The J-2X is an upgraded variant of the storied J-2 rocket engine, which powered the second stage of the Saturn V moon rocket.

FMI: www.nasa.gov/ares, www.nasa.gov/constellation