Apr 232016
 

I’ve never really been much of a fan of the space elevator concept. Not so much that it relies upon nearly magical levels of structural strength (though some new materials are strong enough – at least at small scale – to make the concept feasible), but because it is something of a snail for getting payloads into orbit. If your elevator can climb at a brisk 100 km/hour, and that would be a massive challenge, it will take the elevator about 358 hours to climb to geosynchronous… slightly over two weeks. That’s a couple days in the van Allen belts, so your elevator had better be highly shielded… which means the ratio of payload to climber will be minimal. And then your climber has to either be jettisoned, or it has to make the climb all the way back down. That will be probably several days, during which time you can’t send another climber back up. So you’re probably looking at a turnaround time of around three weeks per “flight.”

Turnaround time can be improved by not going all the way to GEO. Instead, go several thousand miles up, then throw the payload overboard. The higher up you go, the more tangential velocity you’ve have, and the closer to a circular orbit you’ll have. To get into an actual circular orbit, you’ll need to have an onboard propulsion system; the lower your ejection altitude, the more propulsive capability you’ll need. But while this’d speed up the elevator system, it’ll reduce effective payload by *a* *lot.*

Jettisoning a payload puts it into an elliptical orbit with the jettison point being apogee. Perigee rises as the elevator rises; at some point you’ll have an orbit where the perigee is something convenient like 400 km. So all you’ll need is enough propulsive capability to circularize at perigee. But since I can’t be bothered to do the actual math, it seems to me the apogee altitude will be quite high for the elevator, so it might only shave a relatively small fraction off the elevator trip time compared to going all the way to GEO.

Then there’s the problem of actually climbing. How? The cable might be a flat ribbon, millimeters thick by centimeters wide, or it might be actually cable-shaped. But the materials under consideration, graphene and diamond fiber and such, have a little problem: they are virtually frictionless. Run wheels on them all you like, you probably won’t get much traction. Adding a ribbed surface for traction, or adding magnetic materials so a maglev system can haul up the elevator, will add vast amounts of weight to the system.

This video points out some of the engineering issues with the concept:

 Posted by at 7:33 pm
Apr 172016
 

Now available: two new US Aerospace Projects titles.

US Bomber Projects #18

US Bomber Projects #18 is now available (see HERE for the entire series). Issue #18 includes:

  • Boeing Model 726-13: A nuclear powered bomber with the cockpit in the tail
  • Martin Model 164: A pre-war high altitude twin-tailed bomber
  • North American WS-110A: An early concept for what became the B-70, with “floating wingtips”
  • Convair MX-1593: An Early, large five-engined Atlas ICBM concept
  • Boeing Model 701-299-1: The final XB-59 supersonic bomber design
  • Boeing Model 464-72: A B-52 with pusher turboprops
  • Boeing F-15GSE Global Strike Eagle: An unmanned F-15 with a giant missile on its back General Dynamics – Light Weight Attack Configuration 29: An advanced ground attacker with vectored thrust

usbp18ad2 usbp18ad1

USBP #18 can be downloaded as a PDF file for only $4:

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US Transport Projects #6

US Transport Projects #06 is now available (see HERE for the entire series). Issue #06 includes:

  • Lockheed CL-408-15: An early Mach 3 SST
  • Lockheed L-155-4: A very early 8-engine jetliner
  • Boeing Model 754-4V: A very-wide-bodied cargo hauler for Husky
  • Gates Learjet PD1502A: A four-seater with a turbofan
  • Convair Comet Seaplane: An American idea for turning a British jetliner into Flying Boat
  • Lockheed Twin C-5 Shuttle Carrier Aircraft: Two C-5’s mated together to carry a Shuttle between them
  • Boeing Model 765-096 Rev A “SUGAR Volt”: A hybrid jetliner
  • CRC HOT EAGLE – Super Global Troop Transport: Finally, hard data on a rocket transport for Special Forces and Marines

ustp06ad2 ustp06ad1

USTP #06 can be downloaded as a PDF file for only $4:

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And don’t forget…

US Fighter Projects #1 and US VTOL Projects #1 are still new and still available!

 Posted by at 9:44 pm
Apr 162016
 

A sadly tiny illustration of a “Saturn Space Laboratory” from a circa 1960 NASA brochure (promoting the organization to college students). This looks like something halfway between MOL and Skylab; three pressurized modules in a “wet lab” space station. Diameter looks to be 10 feet, same as the Titan booster; early concepts for the Saturn called for the use of the Titan first stage to be the second stage of the Saturn I, with the second stage of the Titan being the third stage of the Saturn. This may well represent a Titan I or II first stage/Saturn I second stage as a space lab.

Given the entertainingly toxic nature of the Titan II propellants, I’d guess this was an earlier Titan I-based concept.

satur space lab

 Posted by at 10:36 pm
Apr 122016
 

A Visionary Project Aims for Alpha Centauri, a Star 4.37 Light-Years Away

A just-announced proposal for a $10 billion program to develop laser-propelled interstellar probes. The idea is to have a mile-wide ground-based array of lasers generate a whopping 100 gigawatts for two minutes to push tiny solar sails with a payload massing about a gram (comparable to the innards of an Iphone). In those two minutes the probe would be accelerated to 20% lightspeed, shooting past Alpha Centauri in about 20 years. It is estimated that Starshot would take 20 years to get going, so, when you factor in the time it takes for the message to get back to Earth, the first photos of A. Cent. from close-up won’t be available until 2060 or so.

The basic idea is not new. Lasers and microwaves have been suggested as “pushers” for sails for decades. Starting in  the 1980s, engineers and scientists such as Robert L. Forward have suggested that advances in computer technology were such that probes could be made trivially small, meaning that it was possible to start considering power systems capable of sending probes to stars at good fractions of lightspeed.

The real trick would be developing a molecule-thick sail that won’t promptly vaporize when hit with a 100 gigawatt laser. This, to me, seems the most difficult part of the project. Next up would making a one-gram payload transmit useful data across the lightyears.

While not mentioned in the article, it seems to me that this vast laser array could, when not shooting microprobes to the stars, be used to power vastly larger launch vehicles into orbit, or perhaps “solar thermal” rockets leaving Earth orbit for, say, Mars.

So far no decent technical details, but the website for the project will supposedly eventually have tech reports.

 Posted by at 10:03 am
Apr 012016
 

This image was passed along to me; it came from an ebay auction from some time in the past. No further info than this illustration, but it is clearly a Boeing “control configured vehicle” bomber concept.

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I know it’s a Boeing design because a year and a half ago I lost out on an ebay auction for another piece of concept art showing the same aircraft, this time with “Boeing” clearly visible on the engine nacelle:

2014-08-03 ebay 1

And I know it’s a Controlled Configured Vehicle because in the early 1970’s, Boeing studied a bomber that was very similar in configuration to this, known as the “CCV-100-2.” There are some obvious differences, such as the cockpit canopies and the engine inlets, but the overall configurations are very similar. The CCV-100-2 received a tiny bit of press in Aviation Week, and was granted a design patent for the overall shape. Sadly, I do not have anything on performance or dimensions; if anyone *does* know more about this, please let me know.

1972-10-16-24

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 Posted by at 12:16 pm
Mar 292016
 

Some photos (from ebay) of a NASA PR glossy from December, 1961, showing the then-current Saturn C-5 configuration. Note the fairly obvious signs of some retouching of the engines on the first stage… either the engines were originally larger, or they were larger in number. Note the lack of the small but distinctive stabilizing fins on the first stage.

saturn c5 3 stages 2 saturn c5 3 stages

 Posted by at 7:46 am
Mar 242016
 

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.

VC-400 Interavia 10-1966 1

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.

 Posted by at 3:29 pm