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#4
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My O-320 powered Long EZ doesn't climb at 10,000 fpm at Vne. ![]() Actually, Rick, the web site says, "Single engine performance is similar to a Lycoming O-320 with constant speed prop." So in that statement they are talking about performance with only one of the two rockets firing. Even so, the statement is not entirely accurate. David O -- http://www.AirplaneZone.com As Dave Barry would say, "an alert reader....".... You are correct in your observation. The more complex and more correct statement is that the single engine ground roll and takeoff are similar to an O-320 with constant speed prop at a low MSL airport. After takeoff, the piston engine/prop thrust drops with indicated speed whereas the rocket engines have constant thrust. Also, the piston engine power drops with altitude. And the reason for the short airshow routine was because the events coordinator asked us to keep it short. Otherwise, Dick would have done a second go-around (which he practiced at Mojave the week before). We landed with about half of the propellants remaining, which was why we did the LOX vent after landing and before rolling into the crowd. Too bad; that second go-around is more impressive at lighter weight. Glide and landing are similar to a standard Long, except that the rocket has less drag (the added fuel tank has less drag than the prop and cooling drag did), and the belly board is less effective ahead of the fuel tank. Dan DeLong XCOR Aerospace |
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