
Hot fire test of Taurus II AJ26 engine – December 17, 2010 – photo courtesy of Orbital
The first stage of the Taurus II launch vehicle is powered by two liquid oxygen/kerosene AJ26 engines, which together generate nearly 740,000 lbs. of liftoff thrust and accelerate the vehicle to a speed of 10,700 miles per hour in the first 235 seconds of flight. As the Taurus II program enters its initial launch phase in 2011, each AJ26 engine will be subjected to rigorous acceptance testing at Stennis prior to being shipped to the Taurus II integration site at NASA’s Wallops Flight Facility in Eastern Virginia. Three more AJ26’s are scheduled for testing over the next five months.


