A photo montage of Boeing display models showing a range of launch vehicles intended to put the early (1959) Dyna Soar into orbit. The three at left are clusters of Minuteman ICBM boosters; the next two are larger solid rocket motor clusters. The next is a Saturn I booster, followed by an all-new recoverable liquid rocket booster, the Titan II and the Atlas/Centaur. The Titan II design was chosen, though it could not actually get the Dyna Soar into a true orbit. To do that, solid rocket boosters needed to be strapped to the sides of the Titan II… leading to the creation of the Titan III.
I am busy at work on US VTOL Projects #3 to be released at the same time as US Fighter Projects #4. USVP#3 is not as far along, but it’s getting there. Here’s a first glimpse:
I thought sure I’d posted this before but… shrug. If’n yer interested in the manned Orbiting Laboratory program of the mid-1960’s, you’ll want to take a gander at the website for the National Reconnaissance Office, which has 825 documents with a total of 20,861 pages on the MOL project:
Index, Declassified Manned Orbiting Laboratory (MOL) Records
A 1966 Boeing concept for a civilian version of the Chinook. Viet Nam veterans I’ve known who rode in Chinooks of that era have stories that make me suspect that *substantial* structural stiffening would have been required for such a craft to be fully accepted by the public; apparently, looking forward towards the cockpit and watching the while cabin twist back and forth was slightly disconcerting. A cruise speed of 200 mph seems slightly optimistic.
Found on the Flickr account of the San Diego Air & Space Museum is this bit of concept art:
The description: “Flaunt Fleet Air Ultra Naval transport sitting 25 above waves on rsbs retractable spar buoy stabilizer concept and design by Thomas P. Faulconer artist Joe Ferrara date 1985 includes plaque and article by designer on back”
This came from an article published in the April 1985 issue of the US Naval Institute Proceedings by Thomas Faulconer, an article I don;t have. So… there ya go.
If you’ve got It, FLAUNT (fleet air ultra naval transport) It. Thomas P.Faulconer. tab lllus US Nav Inst Proc 111:135-139 Apr »85
There have been a lot of “personal air vehicles” designed over the last decade, most designed for VTOL operations and many with purely electric propulsion systems. One such design – which I can’t vouch for on either technical or financial fronts – is the Delorean DR-7 from Delorean Aerospace, founded by the nephew of *that* Delorean.
Their website, lean on details:
http://www.deloreanaerospace.com/
An article from 2017:
A Flying Car From DeLorean Really Won’t Need Roads
And a patent (US9862486B2):
Vertical takeoff and landing aircraft
I’m terrible at posting updates on the latest rewards, but I do get every rewards package out on time. That said, APR Patrons and Monthly Historical Documents Program subscribers have just been sent the rewards for April, 202. This package includes:
1) “Flying Carpet Feasibility Study Submarine Carrier,” a full scan of the 1958 Boeing report on a series of submarines design to carrying Mach3+ VTOL strike fighters
2) “F10F Descriptive Data,” a full scan of a 1953 Lockheed document describing this competitors design
3) Diagram 35-17610, B-52 airdrop carrier aircraft for the Model 844-2050 X-20 Dyna Soar
4) A CAD diagram of a two-stage Rockwell Trans Atmospheric Vehicle using a ground effect machine first stage
If this sort of thing is of interest and you’d like to get in on it and make sure you don’t miss any of the forthcoming releases, sign up either for the APR Patreon or the APR Monthly Historical Documents Program.
All prior “back issues” are available for purchase by subscribers.
The Dyna Soar would, had it been completed, have been the first manned reusable lifting spacecraft. But, sadly, after waaaaay too much money was spent on it, in late 1963 that genius for the ages SecDef Robert McNamara cancelled it and on the same day announced the Manned Orbiting Laboratory… which, after spending waaaay too much money, was also cancelled.
Anyway…
The Dyna Soar was not a “vehicle” like the X-30 National Aerospace Plane which would have its own built-in fully functional propulsion system; nor even like the Space Shuttle Orbiter, which carries the SSME’s and the OMS system. The Dyna Soar was much more akin to the Soviet Buran or the current X-37 in that it was effectively purely a payload, reliant upon the Titan IIIC for launch into orbit, the Titan Transstage for on-orbit propulsion, and a Thiokol solid rocket motor for a de-orbit burn. All it had for its own propulsion was a series of hydrogen peroxide monoprop thrusters for reaction control. It did have a hydrogen/oxygen fuel cell, but it was, more or less, a largely inert chunk of metal. So you might not think that abort would be a big issue, apart from getting out of Dodge if the booster goes high order.
Still, from the beginning of the program and for several years it was planned that the Dyna soar would have not just an ejector seat, but an abort capsule. The entire forward portion of the vehicle would be able to jettison, serving as a re-entry capable “lifeboat” for the lone pilot. By the end of the program the concept had evaporated, being replaced with an ejector seat, and for a good reason: someone finally ran the numbers and realized that an abort capsule added *ridiculous* amounts of weight and complexity to a vehicle already overburdened with weight and complexity. After the Challenger disaster NASA and Rockwell looked at modifying the Space Shuttle with the same sort of jettisonable forward fuselage, and came to the same conclusion that, in essence, “that weighs too much, and astronauts are prepared to take risks.”
The page below from a 1959 report presents artwork depicting the then-current Dyna Soar configuration deploying the escape capsule. It bears a striking resemblance to the McDonnell ASSET test vehicle. This is not accidental, as the ASSET was roughly modeled after the forward fuselage of the Dyna Soar.