NAVWEPS OD-80T-80 
AIRPLANE PERFORMANCE 
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 
Figure 2.21. Climb Performance 
153