Sep 232018
 

Huh. I’m not sure which is more unusual-seeming: that the second-in-command at SpaceX said that they would indeed launch American space weapons… or that it seems odd that an American aerospace firm would even be questioned about such a thing.

SpaceX President Gwynne Shotwell: ‘We would launch a weapon to defend the U.S.’

During an appearance on Monday at the Air Force Association’s annual symposium, Shotwell was thrown a question she said she had never heard before: “Would SpaceX launch military weapons?”

“I’ve never been asked that question,” Shotwell said somewhat surprised. Her response: “If it’s for the defense of this country, yes, I think we would.”

This should be such an uncontroversial point of view that you wouldn’t even expect it to be raised. But we do indeed live in a time different from when Republic advertised their fighters, Boeing advertised their bombers and Martin advertised their nuclear weapons-delivering rockets.

Reminds me of one of the more disturbing moments from my university education. I was in a class on orbital dynamics (of of my favorite subjects back in the day) when we got to ballistic suborbital trajectories: ICBMs, in other words. Who wouldn’t want to study that? Well… turned out half a dozen or so of my classmates decided that they didn’t, and refused to study that section. This baffled both the teacher and myself; but where I saw their position as foolishness worthy of nothing but mockery, the teacher buckled and allowed them to do something else (details escape me). Even if the idea of lobbing nukes to the far side of the world fills you with existential dread, studying the subject is just math. And getting better at the math of lobbing nukes makes you better at… oh, I dunno, getting better at the math of lobbing reusable first stages to land them on floating landing pads.

Vaguely related: promo art from 1961, published in Aviation Week, with a number of corporations proudly proclaiming their involvement in aerospace weaponry.

 Posted by at 5:22 pm
Aug 212018
 

Found on ebay: a piece of B&W art depicting the Saturn V. The provenance is uncertain… unknown where this art originated. There are some unusual details; the tailfins are clocked 45 degrees off, moved from the outer diameter of the engine firings to between them, an odd choice to say the least. The third stage is larger in diameter than the S-IVb with a very long interstage between the S-II and the S-IVb; this *may* indicate that the third stage was meant to be a nuclear stage, with a single NERVA engine attached to the rear of the S-N third stage. The payload is also different: it appears to be a direct lander… no LEM, the Apollo vehicle landed directly on the lunar surface.

 Posted by at 11:34 pm
Aug 182018
 

A piece of Aerojet artwork depicting the NERVA nuclear rocket engine heading to Mars. This is almost certainly artistic license as the vehicle depicted here is a single stumpy upper stage with an aerodynamic fairing. This is mot likely a RIFT (Reactor In Flight Test) configuration, a simple expendable upper stage test configuration meant to be launched atop a Saturn V to prove out the engine.

 Posted by at 10:01 pm
Aug 132018
 

Found on ebay a while back, a pre-NASA Army Ballistic Missile Agency illustration dated 25 May 1959 depicting the Mercury space capsule, including smaller views of it atop both a Redstone and a Jupiter. In both cases this would be a purely sub-orbital lob. It’s unclear just what’s going on with the nose of the Jupiter version; it does not have the abort tower the Redstone version has. This may be a purely aerodynamic fairing, with abort motors located underneath the capsule in the sizable adapter section.

 Posted by at 9:49 pm
Aug 062018
 

Scanned from a 35mm slide at the NASA HQ some years ago. The basic shape here (FDL-7/McDonnell Model 176) appeared on a great many McD designs for the latter half of the sixties from small one-man experimental designs on up to full Shuttle-sized craft like this one. It had both sharply swept fixed wings on the bottom and stowable high aspect ratio wings for landing up top.

 Posted by at 8:25 pm
Aug 022018
 

A piece of color art, scanned from a 35mm slide at NASA HQ some years back. The Lockheed STAR Clipper was an early concept for a reusable 1.5 STO launch vehicle, a  predecessor to the Space Shuttle. The STAR Clipper was described and illustrated in unnecessarily *vast* degree in Aerospace Projects Review issue V3N2 and in US Launch Vehicle Projects #2.

The STAR Clipper was an interesting design which was popular and well known for a while, receiving  lot of kinda-press… it, or shuttles very much like it in appearance, appeared in a lot of publicity art produced by Lockheed, NASA, the USAF and even other companies. For a while it was the Shuttle Stereotype.

 Posted by at 1:22 am
Jul 302018
 

Today, the notion of building a space launch system that uses solid rocket boosters is kinda… silly. Liquids have much higher performance and, as SpaceX has conclusively demonstrated, liquids are quite recoverable and reusable, far easier than solids. But fifty, sixty years ago, solids made a *lot* of sense. They worked, they were reliable, they did not require a whole lot of delicate , constant babying. And for military purposes, they were (and remain) fantastically useful; load them up, stick them in a tube, forget about them for a few years, fire them at a moments notice.

This piece of Aerojet artwork dates from 1961 at the latest and depicts a large solid rocket booster, presumably for space launch. The diameter was 288 inches… larger than the largest actually-tested solid rocket motor at 260″, smaller than the 396″ diameter of the Saturn V (also the diameter of the largest solid rocket motor design I can recall seeing). Note that it uses four nozzles. This is not uncommon on military solids such as the first and second stages of the Minuteman and some sea launched ballistic missiles; it’s costlier and weighs more than a single nozzle, but it give you the same performance at a shorter length. And when your missile is stuffed into a silo or, worse, a submarine, compactness is important. but those missiles all also constrain the maximum dimensions of the nozzle assemblies to be no greater than the motors they are attached to… again, so the missile can fit in a  tube. THIS design went another way, with nozzles well outboard. This precludes silo launch. The advantage for a non-silo launched space booster to split up the nozzles like this is unclear. Some small reduction in total length, and some roll control authority.

Vaguely related: US Bomber Projects #17 has an article and diagrams of a somewhat smaller 260″ diameter solid rocket boosted ICBM from Thiokol.

 Posted by at 6:20 pm
Jul 242018
 

Very late 1950’s Convair promo art of their “Outpost” space-base built from an Atlas launch vehicle. This was publicized enthusiastically by the likes of Krafft Ehricke; it preceded the MOL program, and would have resulted in a  manned facility somewhat similar in size, thought dissimilar in capability. The MOL was a pre-finished, single-launch space lab, while the “Outpost” as a  “wet lab” would have required considerable effort by workers in space suits to finish. To service the Outpost, an Atlas with a Centaur-like upper stage would orbit two wedge-like lifting bodies.

 Posted by at 4:21 pm