0RB JetLab

ENGINE INPUTS

REFERENCE PROFILE

Balanced local demo profile for exploring payload and speed.

01A

ENGINE NAME

MAX THRUST

MAX RPM

RPM

IDLE RPM

RPM

MAX EGT

°C

MAX FLOW

L/MIN

ENGINE MASS

INTAKE Ø

ENGINE Ø

ENGINE LENGTH

FUEL

01B

AIRCRAFT MASS

PAYLOAD

FUEL MASS

WING AREA

M²

DRAG COEFF.

REF. AREA

M²

ALTITUDE

AMBIENT TEMP

°C