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Before the alternative piece, some actual history:
Prior to settling on the SARO P.177 for its high altitude fighter requirement the RN undertook a study that developed a considerably more demanding requirement that might be thought of as a mini OR.329. The following sortie profile for a collision course intercept was outlined:
The AI radar would have to be capable of detecting a mach 1.3 bomber (the expected threat was very roughly analogous to the Tu22) at a range greater than 22 nautical miles under jamming conditions. The aircraft would be under the control of Type 984 equipped ships for much of its interception. For a collision course intercept the air-to-air missile was expected to have a flight time of just twelve seconds but it had to be lethal against the expected threat.
Alternative history:
In reality this requirement does not appear to have made it to industry, but it is fun to imagine that it did and wonder what industry might have come up with. Trying to keep close to the stated requirement does create some significant constraints though. This would be a rocket fighter, so it would have to be configured in such a way that the rocket installation was practical, it was also to be single seat and would have to fit on RN carrier lifts (see the diagram attached of a Phantom on RN lifts for reference) and would have to have various devices to improve take-off and landing performance, e.g. blown flaps and jet deflection as actually included in the P.177 design. Whilst the requirement was more demanding, had it gone forward the RN would have had to have accepted an in-service date of 1965 (planned in-service date for the P.177RN was 1960). Having thought about this, two potential approaches come to mind:
Scaled-up P.177RN: The as chosen design hut scaled up, and built with the appropriate materials (e.g. ICI titanium 314A) to deliver the required performance. The obvious approach would be to design it around the full-size PS.52 Gyron. However, this poses some challenges, the P.177 was already approaching being maxed out length-wise at 50.5ft, with the addition of a folding radome and antenna could be included there is perhaps 2.5-3ft by which the basic design could be lengthened?
Single Seat DeHavilland DH.117 Derivative: It occurred to me that this design, to OR.329, has a very long radome and tandem seating. Some very crude estimates based on pixel counting of the images posted by @overscan (PaulMM) in the DH.117 thread suggest that the radome forward of the antenna gimbal is approximately 10ft and the space taken for the second crewman is approximately 4.5ft. Assuming the nose could be adapted to fold as in the F-4K and Buccaneer, and removing the second crewman allows 14.4ft to be removed from the 66.8ft fuselage length given in the brochure for a total of 52.3ft. That feels like something detailed design could remove, especially as center of gravity considerations and an undercarriage revision to single main wheels would require a redesign and backwards shift of the engine and undercarriage pods. A wing fold would also be necessary. Overall, this feels like an achievable way of getting at something that could meet the above outlined requirement.
Hawker did draw a P.1121 carrier derivative with side-by-side seating so that package could work, but the rocket requirement would be difficult to get right in that airframe - at least the P.1103 installations look less than ideal.
To be clear, this requirement would be much more likely to generate a British XF8U-3 than it would be a Phantomesque type. I am very curious to see what everyone else can come up with!
Prior to settling on the SARO P.177 for its high altitude fighter requirement the RN undertook a study that developed a considerably more demanding requirement that might be thought of as a mini OR.329. The following sortie profile for a collision course intercept was outlined:
- Take-off and turn to climbing course - 0.5 minutes
- Climb to 60,000ft with an end speed of mach 2 - 4 minutes
- Cruise at mach 2 at 60,000ft - 2 minutes
- Turn at 2G or more - 1 minute
- Return to base / marshalling position - 17.5 minutes
- Descent and landing - 25 minutes
The AI radar would have to be capable of detecting a mach 1.3 bomber (the expected threat was very roughly analogous to the Tu22) at a range greater than 22 nautical miles under jamming conditions. The aircraft would be under the control of Type 984 equipped ships for much of its interception. For a collision course intercept the air-to-air missile was expected to have a flight time of just twelve seconds but it had to be lethal against the expected threat.
Alternative history:
In reality this requirement does not appear to have made it to industry, but it is fun to imagine that it did and wonder what industry might have come up with. Trying to keep close to the stated requirement does create some significant constraints though. This would be a rocket fighter, so it would have to be configured in such a way that the rocket installation was practical, it was also to be single seat and would have to fit on RN carrier lifts (see the diagram attached of a Phantom on RN lifts for reference) and would have to have various devices to improve take-off and landing performance, e.g. blown flaps and jet deflection as actually included in the P.177 design. Whilst the requirement was more demanding, had it gone forward the RN would have had to have accepted an in-service date of 1965 (planned in-service date for the P.177RN was 1960). Having thought about this, two potential approaches come to mind:
Scaled-up P.177RN: The as chosen design hut scaled up, and built with the appropriate materials (e.g. ICI titanium 314A) to deliver the required performance. The obvious approach would be to design it around the full-size PS.52 Gyron. However, this poses some challenges, the P.177 was already approaching being maxed out length-wise at 50.5ft, with the addition of a folding radome and antenna could be included there is perhaps 2.5-3ft by which the basic design could be lengthened?
Single Seat DeHavilland DH.117 Derivative: It occurred to me that this design, to OR.329, has a very long radome and tandem seating. Some very crude estimates based on pixel counting of the images posted by @overscan (PaulMM) in the DH.117 thread suggest that the radome forward of the antenna gimbal is approximately 10ft and the space taken for the second crewman is approximately 4.5ft. Assuming the nose could be adapted to fold as in the F-4K and Buccaneer, and removing the second crewman allows 14.4ft to be removed from the 66.8ft fuselage length given in the brochure for a total of 52.3ft. That feels like something detailed design could remove, especially as center of gravity considerations and an undercarriage revision to single main wheels would require a redesign and backwards shift of the engine and undercarriage pods. A wing fold would also be necessary. Overall, this feels like an achievable way of getting at something that could meet the above outlined requirement.
Hawker did draw a P.1121 carrier derivative with side-by-side seating so that package could work, but the rocket requirement would be difficult to get right in that airframe - at least the P.1103 installations look less than ideal.
To be clear, this requirement would be much more likely to generate a British XF8U-3 than it would be a Phantomesque type. I am very curious to see what everyone else can come up with!
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