Page 158 - Aeronautical Engineer Data Book
P. 158
Principles of propulsion 131
VTOL fighter (subsonic)
1 × 22 000 lbf (96.7 kN) turbofan
Military fighter (supersonic)
2 × 25 000 lbf (111.5 kN) reheat turbofan
Launch vehicle solid rocket boosters
2 × 2 700 000 lbf (12 MN)
Fig. 8.7 Aircraft comparative power outputs
