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May 062016
 

A NASA illustration of an advanced solid rocket motor concept, dated 1963. The most obvious difference between the “present” and “advanced” design was the buried nozzle. By properly shaping the solid propellant grain, the motor would perform normally but with a minimum of unused internal volume; this allowed the motor to be substantially shorter than the conventional design. This would make the associated interstage section equivalently shorter, lighter and cheaper. And by shortening and lightening the interstage, the launch vehicle would be shorter, lighter and stronger, with slightly sturdier structural dynamics.

advanced motor

The advantages of a more compact motor like this are pretty obvious. The disadvantages, maybe less so. The most apparent disadvantage is the *need* for far more advanced materials. That buried rocket nozzle is shown to be quite thin, thinner than the “present” design, yet it would be subjected to horrifying heating rates on *both* sides. There are few materials that could withstand that and retain any sort of structural strength.

Additionally: the desire is shown for thrust vectoring. Numerous options for that are available for the conventional nozzle… but it would be much harder with a buried nozzle. It might be easiest to simply gimbal the entire motor. Stop/restart capability has been achieved with solid rockets, but neither design show here provides for that. It is a non-trivial feature.

The igniter is show to be a small rocket motor suspended within the nozzle, directing it’s exhaust forward into the bore volume of the main motor. Variations on this sort of igniter are quite common for relatively short and stubby upper stage motors such as these.

 Posted by at 11:06 pm
May 062016
 

A Falcon 9 first stage successfully landed on a barge out at sea after launching a satellite to geostationary. This was a high-velocity mission that SpaceX did not have high hopes of a successful landing for, yet they succeeded anyway.

This is the third successful landing of a Falcon 9 booster, the second on a barge. The two barge-recovered boosters are to be re-launched at some point. And at some point, the landing and recovery of a space launch rocket will become ho-hum boring. And that will be *awesome.* Because the transformation of a NASA program into boring means a loss of public interest and very likely a program cut; a transformation of a private program into boring means economic success and increased profits and utilization.

Coming soon: the launch of a Falcon 9 Heavy with two boosters, with simultaneous recovery. And at some point, the attempted recovery of a Falcon 9 Heavy second stage. Recovery of one of those would be a whole new level of technical challenge.

 Posted by at 6:45 am
May 022016
 

About three weeks ago I posted video of a device called the “Flyboard Air” which purported to be a VTOL turbojet platform a single pilot stands on. At the time, numerous aspects of the video made it seem kinda fishy, like perhaps it was a hoax, or in some other way not quite what it was claimed. Well, it seems it *is* what it claims. It recently got a Guiness World Record for flying around a harbor in France.

 

 

The “Flyboard Air” has four turbojets (eventually the control system will allow the craft to safely fly on three if one of the four conks out, but right the prototype isn’t up to it) with a total power of about 1,000 horsepower. The inventor wants to incorporate a wingsuit; this would allow the pilot to lean far forward, tilting the thrust from vertical to horizontal and moving the pilot at 180 km/hr. In this record-winning flight, the pilot flew for nearly four minutes, landed… then took off again and did a “victory lap. Total flight time was probably something like 5 minutes, an order of magnitude improvement over the thirty seconds you’d get out of a rocket belt. Potential flight time is given as 10 minutes. You’d think 1,000 horses would guzzle the jet fuel, so I’m a little surprised it even gets that much.

 

 Posted by at 4:00 pm
May 022016
 

A photo of a NASA wind tunnel model of a hypersonic aircraft configuration. The circa 1960 NASA brochure (promoting the organization to college students) that included this provided no further information, but I’m reasonably sure I’ve seen the wind tunnel test report on this, calling it a reusable booster or reusable launch vehicle. If that’s the case, the upper stages and payload were *probably* going to be carried on the things back.

RLV

 Posted by at 8:58 am
May 012016
 

On the one hand:

Can you ram it? Your rights if someone blocks your driveway

In short… if someone trespasses on your property, not only is there basically nothing *you* can do about it, there’s almost nothing the police *will* do about it… because it’s not considered a crime.

But on the other hand…

Pensioner convicted after telling hijab-wearing mother: ‘British women don’t cover up’

If you simply *speak* in Britain, the cops will merrily fine you a reasonably substantial sum.

 Posted by at 10:02 am
May 012016
 

I admit that the USBP series looks kinda… bland. It’s text and line drawings; not a whole lot can be done to jazz that up. Especially since I have no head for graphics design whatsoever apart from layout diagrams.

Still, one reader sent me a mockup of a revised cover of USBP #18:

USBP18blue

Things are moved around a little bit, but the obvious change is the addition of color. The suggestion was also made to consider color-coding each title in the USXP series. Just off the top of my head, I came up with:

Bombers: Olive Drab

Spacecraft: Black

Launch Vehicles: Blue on bottom, transitioning to black at the top

Fighters: slightly bluish gray (like the F-15 or F-22)

Transports: ??

VTOL: ??

The USBP#18 cover was re-done to reflect this, thusly:

USBP18green

Thoughts? Is this more appealing?How about color-coding… good idea or not? And if so, what colors?

I tried something vaguely like this once before, with USBP#05.

 Posted by at 9:43 am
May 012016
 

Or $750/lb. SpaceX pricing for the Falcon 9 and Falcon 9 heavy:

http://www.spacex.com/about/capabilities

capabilities_services_4.29.16_5

For comparison, the Delta IV Heavy costs $375,000,000 with a LEO payload of 28,790 kg/63,470 lbs, or $13,025/kg or $5920/lb.

SpaceX stands a decent chance of monopolizing the launch market in the US. And while the price does not include a Dragon capsule, the US is currently paying the Russians $70 per astronaut to fly on a Soyuz. That’s more than the price of an entire Falcon 9 launch which, with a Dragon V2 capsule, should carry 7 astronauts.

 

 Posted by at 9:17 am