Note according to Milton Thompson they were going to do some neat stuff with the X-20 and it's rocket. For example let the pilot fly the ascent using a fly by wire system.
we haven't tried lately because of how spectacularly the last go DIDN'T work.
I'm sorry, what?
It only goes to suborbital and even an LEO version would have an LEO capability of a few hundred kilograms, perhaps a tonne. Atlas, Delta, Falcon 9, even STS get 20 tonnes regularly.
Atlas, Delta and Falcon charge how many thousand dollars per kilo?
A ticket on a suborbital Virgin Galactic flight would cost 200,000 dollars. Assuming a 100 kilogram human, this translates to 2,000 dollars per kilo. And that's just for a few minutes of suborbital. For $300,000, SpaceX and its Falcon 9 will take you all the way to orbit. So, flight time several times as long, for 50% more cost (and that can go down when Musk gets the Falcon fully reusable).
Dynasoar was an outgrowth of the X-15 program I don't see the CIA being involved thus not much of a factor. I do however see the knowledge that the US vastly out matched the soviets in quantity of nuclear weapons being a big factor in Eisenhower giving the green light to an ambitious manned space program.
The bomber vs ICBM controversy was only a problem just after World War II and Vannevar Bush was largely responsible for that. That could be another PoD about the development of large rockets. But even if the PoD negated the Bush led opposition that still wouldn't get the OP's desire for spaceplane. The best opportunity was when Dynasoar was being developed out of the X-15 program. See Milton O Thompson, At the Edge of Space for a view of the early Dynasoar program.
The divergence that I elude about Nuclear Warhead is about development of the Atlas rocket in the early 50s. When Eisenhower was inaugurated he instituted his "New Look" for america's strategic defense which relied on nuclear weapons.
The big problem was guidance of rockets which was crappy. But with the Hydrogen bomb it wasn't a factor. A miss of several miles meant the target was wiped out. So the question was how much rocket will they need to lift the warhead? And because of Ulam's breakthrough it turned out to be a lot lighter than anybody figured.
By the early 50's the rocket was going to get built. That wasn't the question. Rather how big of a rocket needed was. One of the better accounts of the process can be found in Countdown by Heppenheimer roughly pages 64 to 85. The Atlas big competitor was the Navaho Cruise Missile. But the Navaho has severe technical problems and likely would have never flown.
A Dynasoar was small for a spaceplane only one man to pilot it. Not much room to make it smaller. The program would have been similar to the X-15, run as a series of test flight to gather data. And the big issue of the early Dynasoar program was the booster. With larger ICBM earlier in the inventory one of Dynasoar's problems would have been easily overcome.
As they say in the space program, weight is everything. The Atlas-D did not have much margin. In fact the base Atlas-D could only loft 3,000 lbs to oribt. They had to make a special version for Mercury that could lift 6,720 lbs into orbit. Given the history of weight growth in all the manned program I can't see any of the winged MISS designs being used on the booster of the early 60s.
The Titan 1 developed along the Atlas as a backup only could loft 1,800 lb.
All of these rockets were sized according to the size of the warhead they needed to deliever. Up the size of the warhead a bigger rocket would have been designed. It what happened to the Soviets in the same circumstances.
Note Mercury weighed 4,200 lbs compared to Dynasoar's 11,000 lbs. I studied this quite a bit in creating a switch accurate simulator of the Mercury Space Capsule. (http://www.ibiblio.org/mscorbit).
To summarize then, my point was that with a change of heart by Eisenhower, a more diverse, less focused (and yes, more wasteful...there is always a tradeoff!) move into space would have been possible, which would have allowed a more robust infrastructure to be put into place. Apollo was wonderful in its own way, and I give thanks to God on a regular basis that I was able to watch the first moon landing, but it pushed back any real options for space exploration/exploitation by decades. However, Apollo, political stunt that it was, was the direct outgrowth of Eisenhower's choices in the mid 1950s...by the time that JFK made his speech, the die had been cast...
By the way, I took the liberty of looking at your website...very impressive!
I see and understand your point. I think you have some excellent things to look at for PoDs involving the space program in general. I do agree that Apollo, the Moon Race, and NASA distorted the development of space despite the sheer greatness of their achievement.
My focus was on what PODs would get spaceplanes sooner. My opinion is that you need bigger ICBMs earlier so that Dynasoar could be developed without the delays that happened with the boosters. One way to get that is have the miniaturization of the hydrogen bomb delayed by a few years. As this would have caused a different design to have been adopted for Atlas and Titan in the critical 1951 to 1953 time period. Another PoD would have been for Vannevar Bush opposition to be dropped or overcome which would have started ICBM development sooner. In addition likely there would have been a more diverse efforts with a Bush PoD as there would have been better continuity with the WWII efforts.
Thanks. If you decide to try it make sure use the 2006 edition of Orbitersim not the 2010. It has not been updated for the latest version. Also I have a partially done Gemini. It is physically accurate but uses Orbiter's default control layout to control the craft.
Well, the smallest POD I can think of would be to have Robert A. Lovett accept Kennedy's invitation to be brought into the Cabinet as Secretary of State. From there the X-20 Program "may" survive. Lovett would certainly not be as opposed to it as McNamara, but then again you have two separate space programs running, and in ways competing against one another.
So let us say Lovett allows for the military space program to continue, and even manages to get its budget increased. The X-20 launches as it was intended in July of 1966, and later becomes the main vehicle for the MOL Program. Of course, the Big Gemini could still be developed, and may be required given that the X-20 is not built well as an effective cargo ferry.
Anyway, having Robert Lovett is the simplest scenario I can think of that allows for early development of some sort of Space Shuttle.
1961 May 4 - .
1961 May 12 - . LV Family: Titan. Launch Vehicle: Titan 3C.
- Streamline approach for accelerating the Dyna-Soar program. - . Nation: USA. Spacecraft: Dynasoar. Summary: The Boeing Company offered a "streamline" approach for accelerating the Dyna-Soar program by the elimination of suborbital flights..
1961 May 29 - .
- Martin C plan for Dyna-Soar Step IIA booster. - . Nation: USA. Spacecraft: Dynasoar. Summary: A Dyna-Soar technical evaluation board recommended the Martin C plan for a Step IIA booster..
1961 July 11 - . LV Family: SLS; Titan.
- Advanced Re-entry Technology program and SAINT II program. - . Nation: USA. Spacecraft: Dynasoar; Asset; SAINT; SAINT II. Summary: The Space Systems Division completed two development plans for an Advanced Re-entry Technology program and a SAINT II program..
1962 June 26 - .
- Dyna-Soar designated the X-20. - . Nation: USA. Spacecraft: Dynasoar. Summary: The Department of Defense officially designated the Dyna-Soar glider as the X-20, reinforcing its status as only a research program. The more production-oriented designations XJN-1 or XMS-1 (Experimental Manned Spacecraft-1) were rejected..
I'm sorry, what?
I will make sure to check out your software. I am (as you might have noticed) a huge Gemini fan, so the possibilities that you provide are most appealing...