Jun 162014
 

The flavor of the moment in crowd funding seems to be “Patreon.” The idea is similar to Kickstarter, but instead of a person kicking in X dollars, they kick in Y dollars per month (or per some-sort-of-unit). I tried something similar a few days back with the PayPal “subscription” option next to the tip jar, to results I pretty much expected.

Searching through Patreons listings, I note a number of ‘em for blogs. So… what the heck. Is it worth contemplating for Aerospace Projects Review?

I’ve slapped together a Patreon “campaign,” but I have not yet launched it. However, I’ve stitched together the screenshots of the thing, shown below, listing the “milestones” and the “rewards” I’m considering. In short, I have a fairly good sized library of stuff I’m fairly certain would appeal to a fair number of folks, and this would be a way to get it all scanned and cleaned and posted and whatnot. The way this works, the more an individual contributes, the higher the quality of product they’ll get, and the more the total contributions, the faster the rate stuff will be put out there. The specifics might change, but I think this is a proper sort of setup.

If you have a suggestion or any sort of comment at all, feel free. Advertising, marketing, all that stuff… not my area. So if you see something stupid, or something that could be better, let me know.

patreon

 Posted by at 9:42 pm
Jun 162014
 

At last: Aerospace Projects Review issue V3N4 is available. This issue has 128 pages. The main article focuses on the Boeing Model 844-2050E, the final, almost-built version of the X-20 Dyna Soar spaceplane. Included are not only detailed diagrams showing the design and construction of the spaceplane, but also drawings and information on proposed operational versions, including passenger ferries, satellite inspectors/interceptors, even nuclear bomber versions.

Also included are a large number of all-new diagrams that finally show the Dyna Soar atop the Titan IIIC accurately and in detail, along with proposed variants, variant launch systems and suggested space stations.

An article by Bill Slayton on the Lockheed CL-295 design series. This was a series of tailsitter VTOL fighters including designs derived from the F-104 as well as wholly new designs.

The third article is on the McDonnell F-4(FVS),a mid-1960’s concept to replace the low-mounted fixed wing of the F-4 Phantom II with an all-new variable geometry “swing wing.” The story goes from the F-4(FVS) in its numerous incarnations through the Model 225, McDonnell-Douglas’ entry into the 1968 US Navy VFX contest which resulted in the F-14.

Also, Aerospace History Nuggets on the US Navy SCAT VTOL and the Republic Aircraft RAC-730 SSTO aerospaceplane.

23 megabyte PDF file

 

Here’s the complete issue V3N4 layout:

It is available in three formats. Firstly, it can be downloaded directly from me for the low, low price of $10.00. Second, it can be purchased as a professionally printed volume through Magcloud; third, it can be procured in both formats. To get the download, simply pay for it here through paypal.

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To get the printed version (or print + PDF version), visit my MagCloud page:

http://scottlowther.magcloud.com/

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Also available: the V3N4 Addendum. This contains 49 pages formatted for 11X17. Includes larger and improved versions of all the CAD diagrams produced for V3N4, as well as larger versions of some of the illustrations from the X-20 and F-4(FVS) articles (as well as a number of illustrations that did not appear in the X-20 article):

The V3N4 Addendum can be downloaded for only $4.00!
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 Posted by at 6:07 pm
Jun 142014
 

Here’s another one of those “I was sure I’d posted it before, but now can’t seem to find it” items…

A 1948 promo video by Northrop showing a mockup of a passenger compartment to be built into a B-49-style flying wing. Very spacious, and with one heck of a view to the front and rear, but of course none to the side. The idea of flying wing airliners keeps popping up, but also keeps never happening. There are several decent reasons for this:

1) It’s more difficult to pressurize the non-cylindrical passenger compartment, meaning that it’ll weigh more (and thus negate some of the weight savings of using a flying wing)

2) Configurations like this won’t fit quite so conveniently at most airports. The jetways will have a hard time mating up.

3) Most of the passengers won’t have any sort of view at all, it’d be like flying in a cargo container.

4) The further a passenger is left or right from the centerline, the more disconcerting and uncomfortable rolling maneuvers will be for them.

5) It’s different. The Dash-80 (the prototype for what became the KC-135 and 707) set the basic configuration for the modern jetliner in 1954… 60 years ago. The most modern jetliners don’t really look any different. And like it or not, “convention” matters.

Northrop drawings of this jetliner are HERE.

[youtube JMTwQ9b5hvk]

 Posted by at 9:34 pm
Jun 132014
 

An educational/promotional film from NASA describes the Supersonic Transport program as of 1966. Of interest are the wind tunnel models: they’re are the size of jet fighters. They don’t make ’em like that anymore…

[youtube u9BjJaDlOaQ]

 Posted by at 11:24 pm
Jun 122014
 

Very early. I would be entirely unsurprised if this has no basis in engineering, just artistic license. The “descent stage/ascent stage” ratio seems really, really off. Comes from a NASA PR brochure, date unclear.

See high-rez HERE.

earlylem

 Posted by at 4:57 pm
Jun 102014
 

In the runup to the Saturn program, American aerospace companies studied every possible variation on large launch vehicles. One idea that seemed promising was the use of large solid rocket motors, singly or in clusters, to form large booster stages. It was sensible enough… in the late 1950s large solid rockets were better developed than large liquid rockets. Solids can put out truly monstrous levels of thrust, and reasonably reliably; and they require minimal preparation once stacked up and ready to go. In contrast, liquid rockets are complex and finicky, but with the advantage of substantially higher specific impulse.

In 1959 Lockheed released the results of an early study for NASA on a series of large boosters using solid rocket motors. They studied a range of vehicles, with 2, 3 and 4 stages; 300,000, 1,000,000 and 5,000,000 pound gross weights, and targeting 300 nautical mile circular orbits, geosynchronous, escape and soft lunar landings.

Shown below are diagrams of 1,000,000-pound gross weight boosters using 180-inch diameter solid first stages (440,000 pounds of propellant) and liquid upper stages (LOX/RP-1 or LOX/LH2 for the second stage and LOX/LH2 for the third). Payload weights were given for representative vehicles rather than specific designs.

solids 1

Payload: 39,800 pounds to 300 n.m.; 9,400 pounds to geosynchronous; 12,400 to escape; 3,900 pounds to soft lunar landing

———————–solids 2

Payload: 51,500 pounds to 300 n.m.

——————————-solids 3

Payload: 39,800 pounds to 300 n.m.; 9,400 pounds to geosynchronous; 12,400 to escape; 3,900 pounds to soft lunar landing

——————–solids 4

Payload: 15,000 pounds to geosynchronous; 18,400 pounds to escape; 5,600 pounds to soft lunar landings

 Posted by at 3:34 pm
Jun 082014
 

I’m getting close to being done with this one. The main article, clearly, is the one on the Model 2050E Dyna Soar, the second far smaller article is on the McDonnell F-4(FVS) and derivatives, the third is the old Bill Slayton CL-295 article from the original version of APR. There will be a few more small pieces, not shown here.

v3n4 ds2050e v3n4 cl295 v3n4 f4fvs

Issue V3N5 will almost certainly be smaller than this. Apart from the Lunar Gemini article, it will likely be composed of a number of all-new smaller articles. I’d like to move forward a short article from further down the run to this one, due to having some new info, but that info is embargoed by the source till later in the year. It’d be nice to get back on the two-month schedule for APR, but I wouldn’t hold my breath on that.

 Posted by at 1:13 am
Jun 072014
 

An illustration of the proposed RF-4X from the early 1970s. This was to be a highly modified version of the F-4E Phantom II capable of attaining Mach 3 for short periods. This would be possible by used more advanced inlets with water injection for pre-compressor cooling. The water would be stored in conformal tanks above the fuselage. The RF-4X would be a recon platform for the Israelies, sort of a low-budget, less stealthy SR-71.

rf-4x

More on the RF-4X HERE.

 Posted by at 3:39 pm
Jun 042014
 

Every now and then the notion of a modern version of the Saturn V pops up. It’s a silly idea; even if NASA decided that they needed a functional replica of the Saturn V, they couldn’t afford it. Not because the blueprints are missing; they can be obtained from several sources on microfilm. But the tooling to build a Saturn V is all gone. Many of the materials called for no longer exist. Many of the sub-components come from catalogs that no longer carry them, from companies that folded decades ago. To rebuild the Saturn V would be every bit as hard as building a brand-new vehicle along the same lines, but with modern materials, components and design/manufacturing practices.

Still, the idea of a modern Saturn V seems to appeal to many, including many at NASA. Below is a page from a 2011 Space Launch System presentation showing some of the concepts batted around regarding a modernized Saturn V. Note that the designs shown here were probably not designed in any real fidelity… spreadsheets and Powerpoint is likely as far as most of them got.

2011 SLS

 Posted by at 1:15 am