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 
VELOCITY. KNOTS 
Ftgure P.25. Rangt Performoncr, Jet Aircraft