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ramp weight

    0.02 sec.
ramp weight [′ramp ‚wāt]
(aerospace engineering)
The static weight of a mission aircraft determined by adding operating weight, payload, flight plan fuel load, and fuel required for ground turbine power unit, taxi, runup, and takeoff.


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Sub-classifies the Rollup 3 - A 30" wide driving force, in full-width single-track design, in ramp weight of 6 lbs.
This comparison table provides Citation CJ1+ specifications relative to the Citation CJ1: Citation CJ1+ Citation CJ1 ------------- ------------- Maximum ramp weight 10,800 lbs.
This comparison table provides Citation CJ1+ specifications relative to the Citation CJ1: Citation CJ1+ (preliminary) Citation CJ1 --------------------- ------------- Maximum ramp weight 10,800 lbs.
 
 
 
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