I'm no expert, but I recall they had seen that Nissan had a pretty powerful V6 for IMSA racing and that they could adopt those to air racing, but had many issues trying to keep the motors alive. I think they may have pumped them up a bit higher than race spec too... It has been a long time since reading about it. (The goal for the Pond Racer was to preserve the limited supply of vintage warbirds, this would offer an alternative.)
It was propelled by dual liquid-cooled Electramotive VG30 engines that were derived from Nissan V-6 block engines used in the 300ZX and Maxima automobiles. Fully installed with turbochargers, radiators, and ducts, the V-6’s basic weight increased from 350 pounds to 700 pounds.
The V-6 was also connected to a gearbox which brought the Racer’s wild 8,000 rpm operating speed down to a more propellor-friendly 2,000 rpm. In this respect, the Pond Racer featured four-bladed King Air props that were 80 inches in diameter, and whose knife-thin tips were designed to run at 98% of the speed of sound.
On March 22nd 1991 Dick Rutan took the Scaled Composites Pond Racer out for its first spin in the sky. Commenting afterwards, Rutan noted how the maiden voyage had been a ‘continuous engine emergency’ due to improperly calibrated powerplants.
Over the next couple of trials, the engines were adjusted and recalibrated to work well at moderate power, but even by August, they were still chronically misfiring because the engine control computers were failing to take account of air density.
Another source of trouble was the methanol fuel, which was found to be corroding the plane’s materials and contaminating the oil supply. Consequently, it became standard procedure to drain the fuel systems after each flight and refill them with aviation gasoline in order to safeguard the components from the effects of methanol.
Shoehorning the 195-cubic-inch turbocharged engines into the tight aerodynamic cowlings required compromises as well. And these highly stressed engines were required to run at full power continuously for long periods of time. Oil scavenging and supply issues dogged the aircraft during its three years in competition and resulted in several spectacular inflight failures. Although the engines ran relatively cool on methanol, the composite engine cowlings required the use of external blowers immediately after shutdown to maintain their strength.