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Flight Guidance Systems to be used by the da Vinci Project Tested
Second test of full-scale engines also performed

March 9, 2001

Full-scale Engines ignite to launch rocket for second flight test in New Mexico in March, 2001.

New Mexico, March 9, 2001 - The da Vinci Project reached a second major milestone in its development today in New Mexico. The second test of their full-scale civilian-built rocket engines was completed, launching a rocket for the first time. This allowed the completion of the first test of their newly built flight guidance controls.

Our full-scale engines

This achievement places the da Vinci Project in a good position to move forward with its ultimate goal: to launch a rocket into sub-orbit, twice in two weeks, with rocket scientist Brian Feeney along for the ride. The da Vinci Project recently joined the X Prize competition, which pits non-government-funded projects against eachother in the new race for space. A complete list of the X Prize Rules are available at the competition website.

The 2 engines produce 5,000 pounds of thrust each and are a new generation engineered for lightweight, high reliability and low cost. A complete auto start and multiple scenario abort system are included.

Rocket, in flight

Flight control is achieved through a programmable FAA approved autopilot from a turbine class of aircraft. Outputs feed into the RCS and fully gimballed engines to maintain the attitude and course of the rocket. The pilot would also have two control sticks. One for the RCS and one to control the engine gimbals. Interruption and re-engagement of the auto pilot is done in the same manner as one would when flying an aircraft.

For additional information Contact:

Brian Feeney
416-434-7470
bfeeney@davinciproject.com (more...)