The quad vehicle design is a pressure fed in blow-down[clarification needed] mode from an initial pressure of 320 psi for level 1 (400 psi level 2). The cold gas vernier engines are cross-fed by gas drawn from ullage space of the opposite tank. The vehicle was able to transfer propellant through connecting pipes between opposite tanks by controlling ullage pressures with the thrusters; this helps it balance, minimizing gas use. The main engine had two-axis thrust vectoring. The vehicle was fully computer controlled; with guidance from GPS and fiber optic gyros.
The specification for Pixel/Texel for level 1:
- Width: ~1.9 m (~75 inches)
- Height: ~1.9 m (~75 inches)
- Dry Weight: 650 pounds
- Gross Lift Off Weight (GLOW): ~1500 pounds (360 pounds ethanol, ~500 LOX)
- Payload: 55 pounds
- Engines: 1 (+ 4 cold gas attitude jets)
- Thrust (sl): ~3000 pounds
Engine (XPC-06):
- Thrust: ~3000 pounds (throttleable to 25%)
- Chamber Pressure: 300 psi
- Nozzle Area Ratio: 2:1
- Isp (sl): ~140-~200 seconds (low-high throttle)
- Length: 0.51 m (20 inches)
- Diameter: 0.2 m (8 inches)
- Chamber: carbon fiber reinforced graphite built by Cesaroni aerospace
- Burn Time: >100 seconds, expected >180 for level 2, with approximately double the propellant mass.
Purchase by NASAEdit
On 8 March 2010, Matthew Ross Of Armadillo Aerospace confirmed that Pixel had been converted to methane/LOX propellant and sold to NASA as part of the Project M (NASA) testbed for the Autonomous Landing Hazard Avoidance Technology (ALHAT) LIDAR range finding system under development by Jet Propulsion Laboratory (JPL).
- Young, Kelly (October 13, 2006). "Mock lunar landers to go head-to-head in X Prize Cup". New Scientist. Retrieved 2013-01-04.
- "At NASA, a Quiet Quest to Send a Humanoid Robot to the Moon". New York Times. 1 November 2010. Retrieved 4 January 2013.