A mid-1960’s German (VFW/Heinkel) concept for a VTOL passenger transport, a quad-tilt-wing design, with capacity for 40 passengers or 13,200 lbs of cargo.
I’ve uploaded a two-page article from the era on the VC400. It is in the 2016-03 APR Extras Dropbox folder, available to all $4+ APR Patreon patrons. If interested, check out the APR Patreon.
Seems I’ve sorta fallen off the PDF Review Wagon. So here’s a hastily slapped-together review of a great report (the scans, sadly, aren’t so great, but whatreyagonnado…
V/STOL Concepts and Developed Aircraft. Volume 1. A Historical Report (1940-1986)
Report Number: AFWAL TR 86-3071 Volume 1
Author(s): B. Lindenbaum
Corporate Author: Universal Energy Systems
Laboratory: Flight Dynamics Laboratory
Publication Date: 11/1/1986
Pages: 458
Contract: F33615-83-C-3000
Project: 3038
Task: 303800
AD Number: ADA175379
Photo Enhancement: Complete
Abstract Text:
The purpose of this document is to present a comprehensive, in-depth review of the serious efforts made in the development of VTOL and V/STOL concepts and aircraft other than the helicopter. The time period covered is from the beginning of organized government-sponsored activity in the late 1940’s through the present, during which a very large study and development activity has taken place. Conventional helicopters are not included because their development history is a sizeable subject in itself and one which is already well-documented. Included are V/STOL aircraft which do use rotors but are aimed at providing cruise speeds and aerodynamic efficiencies similar to those of conventional airplanes. Although not aircraft in the conventional sense, wingless VTOL vehicles which use direct thrust (rocket or turbojet/turbofan) for lift in all flight modes also are included since such machines do have a close relationship to some of the more commonly accepted forms of VTOL aircraft. This volume contains an introductory review of V/STOL aircraft concepts and the rationale behind them. The concepts are categorized by propulsion system. This volume contains definitive information and technical reviews of the rocket belt, turbojet/turbofan platform type (wingless) vehicles, and turbojet/turbofan vertical attitude takeoff and landing aircraft.
Two scans of this are available online.
I’ve put scans of a 1968 Popular Science article on the Lockheed AH-56 Cheyenne attack helicopter and a Boeing-Bell brochure on the JVX tiltrotor (which became the V-22) on the APR Patreon dropbox, in the 2016-02 folder.
The Pop Sci article featured cover art by Robert McCall. Just cuz, I tinkered with the cover art, attempting to scrape off the text and restore it to just the painting. Perhaps not a 100% success, but not too bad. The JVX is not *quite* the final V-22 design; a notable difference is the inclusion of a .50 caliber gatling gun in the nose and a rocket launcher hanging off the side the cockpit.
If interested in getting these, please consider signing up for the APR Patreon. The “Extras” are available to all $4 patrons. Quite a pile of high-rez stuff is available now.
One of an extremely large large number of designs put forward for Weapons System 324A, Tactical Fighter X, which eventually became the F-111. This particular design, circa 1962, is the WADD 46 from the Wright Air Development Center and is pretty typical… a twin engine supersonic design with sizable variable-sweep wings.
Two full-rez pages from the WS324A Characteristics Summary have been posted to the 2016-02 APR Extras Dropbox folder for all $4 and up APR Patreon patrons.
I recently acquired diagrams of a B-52 with six high-bypass turbofans. Sadly, the diagram lacks data on *which* engines those were, and when the design was made. So: does this look familiar?
Could be any of several, I think.
The full diagrams have been posted into the 2016-01 folder on the APR Patron Dropbox site. If interested, this and many, many other high-rez aerospace goodies are available to all APR Patreon patrons at the $4 level and higher. So, check it out…
Somewhere north of 20 years ago I received a package in the mail from Martin-Marietta containing stuff on their then-current NIMF study. NIMF was a mangled acronym for Nuclear Rocket Using Indigenous Martian Fuel; basically a propellant tank, structure, landing gear and a nuclear rocket engine, to be used for landing a payload on Mars and for flying or hopping around. The propellant would be liquid carbon dioxide, easily compressed from the Martian atmosphere; the performance would be, by conventional liquid hydrogen nuclear rocket standards, reasonably awful, but it would be adequate to lurch back into Mars orbit or to do long range hops.
Two main designs seem to have been studied: a conical “ballistic” vehicle that would be a dedicated “hopper,” landing on its tail, and a winded vehicle that would land vertically in a horizontal attitude. This latter design was sent to me in the form of diagrams and five computer renders. The renders – early 1990’s vintage – came as viewgraph transparencies, clearly photographs of a computer monitor. The winged vehicle had simple shock absorbers for landing gear, terminating in dishes rather than wheels meaning that a rolling start or stop was impossible. The available information sadly doesn’t explain how the thing was supposed to land vertically.
The full-rez scans of the viewgraphs have been made available to APR Patrons in the 2016-01 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
A NASA illustration (probably from 1964-66) showing the Saturn launch vehicles planned for the Apollo program. Note that the Saturn Ib shows the Lunar Module ascent stage, sans descent stage. This could have led to some interesting mission possibilities.
The full-rez scan has been made available to APR Patrons in the 2015-12 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
Here’s something I have some vague recollection of posting before, but couldn’t find after a cursory search: a sketch of the seating arrangement of a 3-man A-4 rocket (might be the A-8 derivative). This is a scan of a photocopy of a photocopy; the original photocopy was found in the files of a researcher at the NASM twenty or so years ago. It’s thought that the sketch was originally made by Werner von Braun during WWII.
Little data is provided; range is given as 500 km. *Presumably* this would have been a winged, landing-gear-equipped derivative of the A-4; replacing the warhead of the V-2 with just three guys seems like a waste of three guys, as well as a not terribly effective weapons system.
The full-rez scan (such as it is) has been made available to APR Patrons in the 2015-12 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
Just under the wire, rewards for November have been made available to APR patrons. Three documents and one large-format diagram, and one all-new CAD diagram, have been posted:
If you’d like to help out and gain access to these and past and future rewards, please check out the APR Patreon.
A few months ago, Airbus Defence and Space Sas received a US patent for a nearly hypersonic passenger transport. The vehicle has a number of different engines… rocket engines for vertical boost and acceleration, ramjets for hypersonic cruise, turbojets for subsonic flight including takeoff and landing. It would take off conventionally with turbojets, fire the rocket to shoot almost vertically to about 35 kilometers altitude (going supersonic in the process), then level off and cruise under ramjet power at Mach 4.5. The extreme altitude, about 3 times higher than normal jetliner traffic, would mean that the sonic boom should be greatly attenuated by the time it got to the surface.
The wingtip fins would rotate through 90 degrees to maintain center of pressure from subsonic through supersonic.
Unusually for a patent, this one provides dimensions. Fuselage length (dimension 11 in Figure 1) is 52.995 meters; overall length (dimension 110, Figure 3) is 57.63 meters; maximum span (dimension 126, Figure 5) is 27.188 meters.
Interestingly, the design looks like a mishmash of WWII-era designs… the “gothic wing” designed by Michael Gluhareff of Sikorsky merged with the wingtips of the Blohm & Voss P.208-2 or Skoda-Kauba SL-6.
This is US Patent 907661B2. At the moment the Google page for this patent seems a little non-functional; the PDF of the patent won’t download for me. Fortunately, the page for the patent application is functioning just fine. You can download the PDF file of the patent application directly from THIS LINK RIGHT HERE.
Some pages of diagrams:
Here is a video description of the design.
The interior views of the vehicle show one of the problems with rocket-boosted transport aircraft: The majority of the interior volume isn’t people and cargo, but propellant.
Much more aerospace stuff is available via the APR Patreon. If this sort of thing interests you, please consider signing up… not only will you help fund the search for obscure aerospace history, you’ll gain access to a lot of interesting stuff, not available elsewhere.
