Originally posted by Dave Siciliano
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Navy pilot who shot down R MIGs
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Originally posted by Dave Siciliano View PostLooks like that had an engine with 5,000 pounds of thrust. The Citation II I flew had two with 2,500 pounds each. :-)
But what I see is the prototype had 5000 pounds of thrust. The production aircraft had 6250.
And yes, centrifugal compressor engine would spool up VERY slowly, especially from idle. J-69 in the T-37 could take 10 seconds from idle to full power. One thing you checked during preflight was the actual spool up times for the engines in the aircraft you were going to fly. I remember 6 seconds was common.
The T-37 had thrust attenuators to allow you to keep the RPM up around 60% for faster response.
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Originally posted by Dave Siciliano View PostLooks like that had an engine with 5,000 pounds of thrust. The Citation II I flew had two with 2,500 pounds each. :-)
Likely the Citation drinks considerably less kerosene also<g>.
Regards,
Tom Charlton
"The aeroplane has unveiled for us the true face of the earth." - Antoine de Saint-Exupery
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Originally posted by Scott Dyer HPN/NY View Post
How do they work, Terry?
Here is a drawing of one deployed.
When deployed, you kept the engines spooled up, but reduced the thrust. When you got good with the jet, you would "play" the attenuators. Popping them in and out with small throttle movements, without really changing the throttle setting.
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Originally posted by Terry Carraway View Post
1. The early jets were NOT over powered
2. keep the RPM up around 60% for faster response.
re #1 Chuckle, like someone once had said - "NS, L"
and #2 When i was first checked out in the T-33 I distinctly reall being strongly advised/told to - "keep your RPMs up on final so you'll have some response if you need the power!"
best, randy
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