another bit of political history I learned yesterday was the Phantom; re-engined with RR Speys for the RAF and lost a lot of high altitude performance as a result
It's swings and roundabouts.
Compared with the J79
turbojet, the Spey
turbofan had more thrust and had a lower fuel consumption, giving an increase of 10% in operational range, 15% increase in ferry range and better low-level acceleration (improved take-off and climb performance). The exhaust was probably less smoky as well*.
However, the Spey engines had a wider diameter than the J79 due to the bypass ducting, so the rear fuselage had to be heavily modified and the air intakes enlarged to permit the greater airflow they required.
Unfortunately, the increased drag of the engine installation resulted in poorer level flight performance at high altitude.
This engine mod applied to the F-4K (Royal Navy Phantom FG.1) and F-4M (RAF Phantom FGR.2) variants.
Interestingly, the RAF operated some J-79-powered Phantoms as well, having purchased 15 second-hand ex-U.S. Navy F-4J aircraft redesignated F-4J(UK), to use in lieu of the Phantoms deployed to the Falkland Islands after the war.
Crews liked the aircraft, and generally rated them better than the Spey-equipped FGR.2s. They had a slower rate of climb due to the less-powerful engines, but they were also 1,670 lb (760 kg) lighter and able, at altitude, to reach higher speeds (Mach 2.3 at 45,000 ft/13,700 m, compared to Mach 2.1 at 36,000 ft/11,000 m).
Sources used:
1)
F-4 Phantom II non-U.S. operators - Wikipedia, the free encyclopedia2)
F-4 Phantom II variants - Wikipedia, the free encyclopedia3) Article on military aircraft engines written by Bill Gunston and published in the January 2000 edition of AIR International
*
If you ever seen any archive footage of 1950s and 1960s jets, you'll notice just how smoky their exhaust plumes were. The extreme example being B-52s taking off using water injection power boosting.