Though many think of CFR composites as costly, the incorporation of this material into the Vega design might imply that the ESA considers it one of the "advanced low-cost technologies" mentioned on its Website as being used in the new launcher.
According to presentations at the CarbonFiber 2011 conference late last year, carbon fiber is becoming more plentiful and can meet demand in aerospace and other high-performance applications, in part because new suppliers have entered the market. And at least one marker research firm's presentation said that high-rate CFR composite manufacturing methods are helping to increase the supply of composites, and that CFR composites are on a path to becoming the dominant material in aircraft structures.
In addition to using composites in the Vega launcher, the ESA is keeping manufacturing costs down by using prebuilt production facilities for its line of larger Ariane launchers. The single-body Vega has been designed with three solid propulsion stages and a liquid propulsion upper module used for attitude and orbit control and satellite release. The maiden launch occurred at the Guiana Space Centre in French Guiana, where it completed a flawless qualification flight.
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Thanks, Dave, for all that info on potential dangers of composites, as well as the info about the lack of dangers in some cases. I agree, the unintended consequences of a new technology must be carefully considered before its implementation.
@3drob: You're right about carbon fibers causing a skin rash. It's not particularly serious from a medical perspective, but apparently it can cause a world of discomfort.
You're also absolutely right that it's important to consider all kinds of possibilities when evaluating a new technology.
Believe it or not, NASA actually did a study regarding the possibility of damage to electrical and electronic equipment resulting from the crashing of commercial airliners with carbon-fiber reinforced parts. Carbon fibers are electrically conductive, so presumably if they are released in the atmosphere after a crash, they could get into ground-based electronics and cause shorts. NASA did a fairly detailed analysis and concluded that this was very unlikely.
A lot of work has also been done on how carbon-fiber reinforced composites break up during atmospheric re-entry. This is actually something that's fairly well understood, since one use for carbon-fiber reinforced composites is as ablative barriers (where the break-up of the composite protects a capsule on re-entry).
Dave Palmer answered my question about inhalation dangers. I've heard from people that work with it that while fiberglass fibers work their way out of your skin, carbon fibers tend to work back into the skin (so the disintigration in atmosphere could be a source of polution).
My other question was centered on the idea that objects constructed of carbon fiber are fundamentally more durable than those constructed of standard materials. The assumption with a booster is that it will disintigrate on use (unlike prior applications like planes, well, at least hopefully planes). If so, they may not disintigrate as assumed and could become a hazard to earth bound objects (myself included). Even if they disintigrate, they may not become small enough pieces to be harmless. How durable are carbon fiber materials?
It wouldn't be the first time some game changing technology was introduced by Engineers who didn't re-examine long held prior assumptions.
@3drob: Inhalation of carbon fibers is not really all that dangerous, at least as far as inhalation of foreign substances goes. (When it comes to carbon nanotubes, it may be a different story). At any rate, the airborne concentration of carbon fibers produced by re-entry of a launch vehicle is likely to be extremely small -- the earth's atmosphere is really big, and fibers are likely to be widely dispersed by the time they reach ground level. Inhalation hazards are more of a concern for people working in composites manufacturing, where it is important to have adequate personal protective equipment.
Chuck, composites have been used in launchers before, but not for the entire shell. The reasons for their use are basically the same ones as in other aerospace apps: light weight and toughness. CFR composites just keep getting stronger. Here's some info from Hexcel:
This slideshow includes several versions of multi-materials machines, two different composites processes including one at microscale, and two vastly different metals processes. Potential game-changers down the line include three microscale processes.
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