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Old 19th Sep 2010, 02:51
  #755 (permalink)  
riff_raff
 
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According to this article, maintaining 250kts required 1300hp from the T800, leaving 300hp in reserve.

Sikorsky engineers say the company's self-funded X2 advanced technology helicopter could reach 265kt (490km/h) or more in the next few months after a central sail fairing is installed on the rotor mast.
The twin coaxial contra-rotating rotor demonstrator reached its project goal speed of 250kt in level flight during a morning test flight on 15 September in West Palm Beach, Florida.
At that speed, test pilot Kevin Bredenbeck says the T800-powered pusher had a reserve of around 300hp (225kW), although test limits held the speed to 250kt, a programme target speed achieved about midway through the 1.1h flight. Total power required to maintain 250kt was 1,300hp, 80% of the T800's capability.
In slightly over two years of testing, the X2 has flown for 16.2h on 17 flights, far exceeding the maximum level cruise speed for a helicopter to date - officially 217kt by a Westland Lynx, and unofficially 236kt by the company's XH-59A demonstrator in the early 1970s.
Sikorsky is investigating whether to attempt an official speed record during the final flight-testing on the vehicle, which is likely to involve two flights for acoustic testing and two flights for sail fairing and higher speed testing.
Steve Weiner, chief engineer for the X2 programme, says the stationary sail fairing, sandwiched between the two main rotors, could add 15kt to the cruise speed, once engineers perfect the installation.
Ground tests of the fairing are to start in the next few weeks.
Weiner says Sikorsky is investigating whether to attempt an official speed record during the remaining testing on the vehicle, which is likely to involve two flights for acoustic testing and two flights for sail fairing and higher speed testing.
The CTS800-5 used in the X2 is rated at 1681hp for take-off. And there is always the hot rod modifications of water or nitrous injection sometimes used for temporary power boosts. So the X2 might be capable of substantially more than that 250kts. At least if Sikorsky is willing to trash an engine to get there......

To answer widgeon's question on fuel burn, the published SFC of the CTS800-5 is about 0.49 lb/shp-hr at MRP. Which means the X2 was burning about 637 lbs/hr at 250kts.

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