Atlantic Navigator Mission Performance

The following form is used to estimate the mission performance of the Atlantic Navigator aircraft.
At the moment, the following assumptions are made in the analysis below:

Note that the required flight distance is 3630 statute miles or 3150 nautical miles. (great circle no wind).


Geometry

Span:(ft)
Wing Area:(sq ft)

Drag

Wing Section CDp:
Non-Wing f: (sq ft)

Structures / Weights

Take-off Weight: (lb)
Payload Weight: (lb)
Engine Weight: (lb)

Propulsion / Power

Shaft Power: (hp)
BSFC: (lb/hp/hr)
Prop efficiency: (lb/hp/hr)

Conditions

Initial Altitude: (ft)
Initial Speed: (kt)
Final Altitude: (ft)
Final Speed: (kt)
Take-Off Speed: (kt)

Results

Range:(n.mi.)
Endurance:(hr)
T.O. Wing CL:
Initial Wing CL:
Final Wing CL:
Initial L/D:
Final L/D:
T.O. Climb Rate:(ft/min)
Zero fuel weight:(lb)
At the moment, this page is not linked so ignore the comments below.
Click the Get Inputs button to load the values currently available from other groups.
Click the Compute button, to do the calculation via javascript.
Submit sends the listed inputs and results to the server for use by other groups.
Eventually submit will require design review and explanation, but for now anyone can change anything.