NAVWEPS 00-8OT-80  AIRPLANE PERFORMANCE  GENERAL RANGE CONDITIONS  TURBOJET  THRUST  REO ’ D  LBS  THRUST  REO ’ D  LBS  THRUST  REP ’ 0  LBS  MAXIMUM  ENDURANCE  MAXIMUM  APPLICABLE  FOR  A PARTICULAR  -WEIGHT  -ALTITUDE  -CONFIGURATION  VELOCITY, KNOTS  EFFECT OF GROSS WEIGHT  CONSTANT  ALTITUDE  t  EFFECT OF ALTITUDE  .%A LEVEL  SEA LEVEL  AT ALTITUDE  /  CONSTANT  WEIGHT  7  VELOCITY. KNOTS  c  Ftgure P.25. Rangt Performoncr, Jet Aircraft 