Sep 122016
 

Jeff Bezos of Blue Origin has described a new rocket his company is working on , the “New Glenn.” It’s kinda big:

new-glenn-large2

The “New Glenn” will be 27 feet in diameter (close to the Shuttle External Tank, it seems), 270 feet tall in a two-stage configuration and 313 feet tall in a three stage configuration. The first stage is recoverable, landing vertically under rocket power. It will have seven BE-4 engines burning natural gas and oxygen, producing 3.85 million pounds of thrust. The second stage uses a single BE-4 engine with an increased expansion ratio. The third stage uses a LOX/LH2 BE-3 engine.

The article says that Bezos has claimed that the rocket will fly “within the decade.” If that means by the end of 2019, that’s pretty ambitious.

 Posted by at 10:00 pm
Sep 052016
 

Produced by Bell Aerospace around 1960 as a promotional item was this “ticket” for a flight from New York City to Melbourne, Australia. The aircraft shown was a two-stage hypersonic passenger transport; the first stage was essentially a supersonic transport equipped with turboramjet engines; it carried on its back a rocket powered passenger spaceplane. At the time it was pushed by the likes of Walter Dornberger, who had previously publicized a two-stage all-rocket powered hypersonic transport. There was some link between this design and the Dyna Soar program, but it is unclear just how involved the engineering was on the HST. Artwork was produced and a good display model, but it’s hard to tell if it went any further than that.

bell hst ticket 2 bell hst ticket 1

I have uploaded high-rez scans (600 dpi) to the 2016-09 APR Extras folder on Dropbox. This is accessible to all APR Patreon patrons at the $4 level and above.

 Posted by at 1:11 am
Sep 032016
 

Several days ago word hit of someone with six file boxes of their fathers stuff, wondering what to do with it. Not an unusual occurrence. But in this case, the father was an important engineer  at North American Aviation, worked on the XB-70, B-1 and Shuttle, and the files all related to that. In the end, the archive wound up on Craigslist, and sold shortly afterwards. It is now being shipped… to me.

I would not have been able to afford the archive – never mind the shipping costs – on my own. However, by working with the patrons on the APR Patreon , we were able to pool funds so that the total cost per person is *trivial.* When the archive gets here – all 300+ pounds of it – I will go through every single page and catalog it; the best stuff will be scanned and, barring ITAR & classification issues, all of the crowdfunders will receive the complete set of high-rez scans. And then when I’ve gleaned from it what’s worth gleaning, it will be donated to an appropriate archive… the Smithsonian, the SDASM, the National Archives, Edwards AFB, whatever seems best in the end.

The door to sign up for this crowdfunding project is now closed. It followed shortly on the heels of a similar project that scored an admittedly much smaller but definitely fascinating  collection of F2Y Sea Dart documentation and diagrams, including much about operational follow-on attack aircraft meant to operate from ships and subs; and a similar archive that was crowdfunded a year or two back that scored a whole bunch of 2707 SST stuff. I’ve grown sick of seeing amazing stuff appear on ebay and then vanish into a black hole, never to be seen by anyone again; this way, aerospace history is preserved and shared.

If you’d like to be involved in this sort of thing, sign up for the APR Patreon and you’ll not only get the monthly aerospace goodies that comes with membership, but you’ll also be able to get in on these crowd funding efforts. You’ll save aerospace history, get a bunch of amazing stuff, and not have to spend a whole lot to do it.

 Posted by at 8:05 pm
Aug 302016
 

In the previous installment I worked out what I think the diameter of the individual modules is on the very large Lockheed Space station in this piece of art:

At the time I devoted my efforts to diameter and just kinda half-assed the module length. Now behold, in this latest installment of Don’t You Have Anything Better To Do Theater as I work out the module length with greater precision and less guesswork, using image processing programs (specifically Paint Shop Pro) and CAD programs (specifically Rhino 3D).

Continue reading »

 Posted by at 3:15 pm
Aug 292016
 

Military hardware design programs often have code names that are random or nearly so, so you can’t figure out what they are if you overhear them. Concepts like “Have Blue” or “Copper Canyon” or “Science Dawn” or even “Silver Bug” are pretty opaque. But every now and then there are concepts like Avro Canada’s 1960 idea for a truck capable of carrying and launching two Minuteman ICBMs: “Big Wheel.” For once, the name matched the product.

bigwheel

One wonders what sort of career these might have had in the Monster Truck circuit after they became obsolete.

This is a document I scored off ebay a little while back; it arrived and I’ve scanned it and will include it in the very next APR Patreon catalog. If you’d like a copy, a monthly contribution of as little as $4 will get you the full-rez 300 dpi scan of each months reward documents and diagrams… currently, three documents, one large-format diagram or piece of artwork. That’s a buck an item. Give the APR Patreon a look.

bigwheel layout

 Posted by at 7:26 pm
Aug 272016
 

Earlier this year I posted this image of a late 60’s/early 70’s Lockheed space station:

And asked if there was any hard data out there on the design. Much to my disappointment, but not to my surprise, there doesn’t seem to be any. Clearly the artist devoted a considerable amount of effort to the project… it’s not something slapped together on a whim. But it’s also likely something that got buried and may never again see the light of publicity. So some months back I decided to try to figure out just how big it was supposed to be. Fortunately there are reasonably clear humans for scale.

First off: one thing you discover real fast about the world of concept is art is Do Not Trust Scale References. Things aren’t scaled *down* too often, but things are scaled *up* with annoying frequency. Because Bigger Is Better, I suppose. Consequently, the artist here *could* have taken serious liberties; scaling things up by a factor of 1.5 or even two would not be unheard of. But… this is seemingly all there is. Without further data, you have to work with what you have.

So, starting with the cutaway image, there are a number of male human figures. Assume that the average is about 70 inches tall (for those of you in countries that *didn’t* land men on the moon, 70 inches is about 5.7621e-17 parsecs). Three figures are fairly clearly visible on the uppermost module… one is 67 pixels tall, one is 69 pixels tall and one is 77 pixels tall. The average there is 71 pixels. Thus… 71 pixels = 70 inches. For simplicity, let’s just assume that 1 pixel equals 1 inch.  The diameter of the module can be estimated based on the top and bottom points of the cylinder. The top  is clearly visible via the cables entering into it;  the underside has similar cables which are not visible due to the module being slightly rotated. If we assume that the bottom is as far from the visible edge as the top is, that gives a diameter of 386 pixels, or 386 inches.

module 1 dims

Interestingly, and perhaps tellingly, the diameter of the Saturn V first and second stages was 396 inches. I think it’s perhaps safe to assume that we’re looking at modules designed to be that same diameter. Drawing one of the modules in CAD by tracing over the geometry gives a module length of about 1116 inches.

lock station module

Coming up next time on “Don’t You Have Anything Better To Do Theater:” the overall layout and dimensions of the space station.

 Posted by at 3:37 pm
Aug 242016
 

An early/mid 1960’s concept model of an interplanetary spacecraft using a nuclear fusion powerplant. Back then there was a LOT of faith in the idea of fusion reactors being just around the corner. One very obvious design flaw? No radiators. Any internal-fusion system (or internal-fission, for that matter) would need *vast* radiator surface area.

Details on the photo are unavailable. I originally downloaded this image from the GRIN (Great Images in NASA) website, which has now been closed in favor of a Flickr account that is difficult to search. Feh. If you want the full-rez version *another* Flickr account has it HERE.

GPN-2009-00027

 Posted by at 5:12 pm
Aug 242016
 

A NASA-Langley film from decades ago, a collection of quick clips from wind tunnel tests. These show models designed to bend and flex somewhat like their larger real-world kin, and then they are massively overstressed to the point of failure. If doing a spit-take was a real thing rather than a Hollywood trope, I woulda spit-took at about 1:20, when a Boeing 2707-100 supersonic transport model is shown being turned into a damn porpoise in the wind tunnel (instead, I just blurted out “holy shee-it” and laughed for a while). About 15 seconds later it (or a model similar to it) is turned into so much confetti. I assume the wind tunnel had some sort of shrapnel-filter to keep the junk from being sucked into the blades…

 

 

 

 Posted by at 2:17 am
Aug 222016
 

The Ryan XV-5A Vertifan was a 1960’s VTOL aircraft that was given considerable testing and proved to be reasonably successful, yet it was not chosen to be put into production. he video below (a couple different versions of it) show the XV-5A being put through its paces. It’s shown to be a remarkably nimble and stable platform. Also shown are numerous pieces of concept art, the XV-5A being used in a rescue capacity. Interestingly, the idea presented was to send the VTOL right alongside strike aircraft so that it would be right there on the scene ready to collect any pilots who happen to get shot down during the mission.

The XV-5A used largish fans embedded win the nose and wings to provide vertical thrust; the fans were driven by the exhaust from the jet engines. This is not a particularly elegant solution, unlike the Harrier with its fully integrated single engine system, but the fan approach would provide both better fuel efficiency during hover and lower jet velocity compared to something like the Harrier or the F-35. This would mean that the vertical thrust would tear up the dirt or deck plating a whole lot less.

One wonders how well the XV-5A would perform today. It would have the benefit of better engines and better materials, meaning more thrust at lower fuel consumption, in an aircraft that weighs less. And perhaps more importantly, modern avionics and computerized controls would make this plane much more stable, controllable and safe in hover.

 

 

 

 Posted by at 9:09 pm