This is why it is jetpunk; steampunk, to achieve the Coolness factor, simultaneously exaggerates the potentials of Victorian tech and unrealistically ignores the alternative techs that did evolve OTL to supplement and succeed them.
It is one thing to temporarily delay the development of rocketry compared to a OTL, a little bit, to give projected developments looked to in the 1950s in airbreathing jets a little bit more time to evolve. But sooner or later someone will get back to the rockets, if only for ballistic missile purposes, and a missile that can achieve intercontinental ranges is just a step away from a rocket that can put something into orbit. To delay that for decades, in favor of dubious approaches to airbreathing all the way, or even air-launch of rockets, involves handing both the US and Soviet military-industrial complexes the Idiot Ball. Even this timeline, IIRC, has the Chinese picking up the rocketry slack; once that happens the Pentagon and Kremlin have no more excuses left; too bad it makes supersonic bombers obsolete and totally changes the game for aircraft in general.
Even going supersonic for air-launch, an idea I muster more enthusiasm for than the better-educated in these matters e of pi, never seems to work out no matter how much I want it to. I don't think the whole business of merely counting on getting into thinner stratospheric air for marginally better rocket engine performance is worth it at all; adding speed to reduce the delta-V the rocket stage(s) need to reach is more helpful.
But unfortunately not so helpful that, if you look at with hardnosed economy rather than romantic eyes, it makes much sense to make say a Mach 3 launcher plane compared to the alternative of simply achieving the necessary speed and altitude for the upper stage or stages by stacking them on top of a suitably large and powerful booster stage launched from the ground. Sure, the air at the ground level is thick and not only creates significant drag but worse, impedes the exhaust of the rocket, thus robbing it of both thrust and specific impulse just when one wants both the most. Too bad; it costs 20, maybe 25 percent more than if the rocket were operating in hard vacuum--so you up the thrust of the engines and mass of the fuel, and punch on through anyway. It only takes a minute or two to match and exceed what the best high-supersonic launch plane we could possibly build could accomplish.
The chief difference is, the launcher plane--if we could build it--would be reusable. It had better be! If it is going to launch anything big though the all-up takeoff weight is going to be huge, in the range of a thousand tonnes or more, or three times bigger than anything that has gotten airborne to date, so it will not be able to operate from just any old runway.
Nowadays there is a lot of talk about making booster stages of rockets reusable too. Even if not--it is a question of volume, whether building a throwaway booster, most of whose mass is propellant, works out to be more or less expensive than the development cost and infrastructure of a suitable launch aircraft. And most booster first stages will shove the upper stack to both altitudes and speeds that exceed even the most ambitious airbreathers that can realistically be anticipated---with 21st century tech!
BTW if e of pi is right that the top speed of a realistic scramjet is just Mach 4 I don't see the point in developing them at all; by the early 1960s the USAF had two aircraft that could come near to matching that speed using engines much more conventional than scramjets! And the Soviets soon came near to matching these speeds themselves.
It is one thing to temporarily delay the development of rocketry compared to a OTL, a little bit, to give projected developments looked to in the 1950s in airbreathing jets a little bit more time to evolve. But sooner or later someone will get back to the rockets, if only for ballistic missile purposes, and a missile that can achieve intercontinental ranges is just a step away from a rocket that can put something into orbit. To delay that for decades, in favor of dubious approaches to airbreathing all the way, or even air-launch of rockets, involves handing both the US and Soviet military-industrial complexes the Idiot Ball. Even this timeline, IIRC, has the Chinese picking up the rocketry slack; once that happens the Pentagon and Kremlin have no more excuses left; too bad it makes supersonic bombers obsolete and totally changes the game for aircraft in general.
Even going supersonic for air-launch, an idea I muster more enthusiasm for than the better-educated in these matters e of pi, never seems to work out no matter how much I want it to. I don't think the whole business of merely counting on getting into thinner stratospheric air for marginally better rocket engine performance is worth it at all; adding speed to reduce the delta-V the rocket stage(s) need to reach is more helpful.
But unfortunately not so helpful that, if you look at with hardnosed economy rather than romantic eyes, it makes much sense to make say a Mach 3 launcher plane compared to the alternative of simply achieving the necessary speed and altitude for the upper stage or stages by stacking them on top of a suitably large and powerful booster stage launched from the ground. Sure, the air at the ground level is thick and not only creates significant drag but worse, impedes the exhaust of the rocket, thus robbing it of both thrust and specific impulse just when one wants both the most. Too bad; it costs 20, maybe 25 percent more than if the rocket were operating in hard vacuum--so you up the thrust of the engines and mass of the fuel, and punch on through anyway. It only takes a minute or two to match and exceed what the best high-supersonic launch plane we could possibly build could accomplish.
The chief difference is, the launcher plane--if we could build it--would be reusable. It had better be! If it is going to launch anything big though the all-up takeoff weight is going to be huge, in the range of a thousand tonnes or more, or three times bigger than anything that has gotten airborne to date, so it will not be able to operate from just any old runway.
Nowadays there is a lot of talk about making booster stages of rockets reusable too. Even if not--it is a question of volume, whether building a throwaway booster, most of whose mass is propellant, works out to be more or less expensive than the development cost and infrastructure of a suitable launch aircraft. And most booster first stages will shove the upper stack to both altitudes and speeds that exceed even the most ambitious airbreathers that can realistically be anticipated---with 21st century tech!
BTW if e of pi is right that the top speed of a realistic scramjet is just Mach 4 I don't see the point in developing them at all; by the early 1960s the USAF had two aircraft that could come near to matching that speed using engines much more conventional than scramjets! And the Soviets soon came near to matching these speeds themselves.