w SIN ,--  COMPONENT  OF WEIGHT  ALONG FLIGHT PATH  THRUST  -  -  --  __----  AVAILABLE  AVAILABLE  AND  JET ACFT  THRUST  REOUIRED  LBS.  POWER  AVAILABLE  AND  POWER  REolYLRED  VELOCITY, KNOTS  l= ‘ a JET  Pr, POWER REOUIRED  POWER AVAILABLE  PROP ACFT  SPEED FOR MAX R.C., JET  SPEED FOR MAX R.C., PROP  I  VELOCITY, KNOTS  NAVWEPS OD-80T-80  AIRPLANE PERFORMANCE  Figure 2.21. Climb Performance  153 