Aracnid, I really appreciate you saying that. When I'm writing these, I tend to think I'm doing it only for myself, but then you say something like that and it inspires me to do the next one.
I agree with Bill Cameron's analysis, except that the Howitzers could conceivably be used in the war, even if only in an attempt to justify the massive expenses by showing that the weapon is at least operational, and not just a money-drain.
Maverick,
Exactly.
They'll be used if only to justify the expense, but there will be no real use of the "Howitzers". That is, there will be no use in a militarily significant manner.
Bill
Well if you take the words of Amerigo that "it was ( in past ) the weapon that ended the war " your analysis is a bit off ...
Err... no. Alumin(i)um has a density of 2.7, Titanium 4.5. Titanium is only marginally lighter than steel, actually.Titanium was much stronger than aluminum but had roughly the same weight.
Exactly, although we cannot assume (or outright deny, either) the possibility that Amerigo has a plot twist and that the weapons could end the war, in a way that is to us inconceivable for the time being.
It says "ended" the war, not "won" the war.
Vagueness is always key when Foreshawoding..
??? Gyroscopes are fine. No problem with them. The Nazis put them in V2s (you might even be engaged in overkill here, I'm not sure). So, knowing which direction they're headed is easy. But you haven't addressed the needed accelerometers (unless I missed something), and integrating distance based on acceleration is ... non-trivial for the time.The first part of the guidance dilemma ... I'm sure you'll let me know what I got wrong.
***
In the broadest sense, control consisted of two components: navigation and steering. Some initial work was done on external missile control, but this proved unfeasible in light of the long range of the Howitzers and the possibility that an enemy might intercept the steering commands and somehow jam or alter them. It was decided at an early date to have both control components internal to the missile. Thus, the problem became how to design a missile that could automatically detect where it was, then automatically alter its course as required. In modern rockets, this is done with high-speed onboard computers that determine if course corrections are needed in fractions of a second. No such techniques were available in 1943, and few people even thought such a thing was possible at the time.
The test rockets fired by Goddard and the other Oak Canyon scientists used gyroscopic stabilization to keep their rockets moving upward. This technique, however, did not immediately lead to success at longer ranges or under control. When used on the Rifle, the midsized rocket used for testing new techniques and approaches to be applied to the Howitzer, it was discovered that the strong vibrations caused by the Rifle’s more powerful engines were transmitted through the gyroscopes’ mountings, causing the gyroscopes to be forced away from their proper orientation. Enter Charles Stark Draper, founder of MIT’s instrument lab. In the first two years of the war, he developed a sealed gyroscope for use on antiaircraft gun emplacements, which had to deal with enormous vibrations as they were fired. In the first live-fire test of these stabilized AA guns, the battleship South Dakota downed no fewer than 39 Japanese aircraft, setting a record that still stands for a single battle. This achievement, which took place during the heated battles around Guadalcanal, brought Draper’s work on gyroscopes to the attention of the people in Oak Canyon. He was brought into the project with most of the other instrument lab people toward the end of 1943 and put to work on the guidance problem.
Through fits and starts, he came up with a unique solution. For the precise guidance needed, the gyroscope had to spin on fine jeweled bearings. But in order to cope with the stresses of rocket flight, the gyroscope had to be built sturdy enough to withstand vibration. The fine bearings couldn’t hold the weight of the sturdier gyroscope, which left Draper with an unsolvable problem. Faced with an insurmountable obstacle, he followed a military maxim and outflanked it. Rather than alter the gyroscope or the bearings, he encased the entire setup in a canister and suspended the canister in a fluid to reduce vibration. Thus, the gyroscope could rotate freely as required, and the bearings would not have to support the weight of a gyroscope built to withstand vibration — the fluid would take that role. Manufacturing these fluid-encased gyroscopes proved yet another engineering challenge, however.
Draper and the Manhattan Project contracted out to Sperry Gyroscope Company of New York to build the new fluid-encased gyroscopes. Sperry was one of the largest gyroscope manufacturers in the country, and it had worked with Goddard before the war on gyroscopes for his rockets. Furthermore, James Webb, its vice president, was an enthusiastic member of the American Rocket Society, from whose ranks the Manhattan Project recruited many scientists and engineers. Though Sperry was already building gyroscopes for the famous Norden bombsight and antiaircraft gun emplacements for both branches of the U.S. Military, it agreed to accept the contract to build Draper’s new design. An entirely new factory was designed and built in Connecticut, and this facility produced virtually all of the gyroscopes for both Howitzer models until the 1950s. Because the jeweled bearings and the fluid encasing the gyroscope canister were sensitive to contamination, the entire assembly had to be put together in a clean room. The cleanliness demanded went far beyond anything in a large-scale American industrial production to that point: the air was filtered four times, through progressively smaller filters; the assembly room was pressurized to keep outside air from entering; employees entered the assembly room through an airlock; all were required to change into special clean suits before beginning their work.
When the first of the fluid-encased gyroscopes came off the assembly line, new problems were revealed. The fluid had to be heated slightly and it had to maintain a consistent temperature in order to zero the canister’s weight on its bearings and to prevent variation that might throw off the finely calibrated gyroscopes. Constant electrical voltage had to be arranged, and special line conditioners were installed on the cables leading to and from the gyroscopes. Each had to be calibrated and aligned perfectly, as three gyroscopes were needed in each rocket: one each to control pitch, yaw, and roll. Each had to work with the others in perfect harmony, otherwise small imperfections could cause large errors in control.
Ideally, a guidance system would incorporate some form of location detection and a computer able to calculate the appropriate action needed to correct for any course imperfection. Unfortunately, the state of computer technology during the war years meant that any computer capable of these calculations would weigh far more than the entire predicted payload of the Howitzer. In addition, the fragile vacuum tube-based electronics of the time couldn’t withstand the intense vibration of rocket flight, regardless of their complexity. As before, Draper was forced to sidestep the issue. Because the Howitzers would be unable to recalculate their trajectories based upon outside input, he built his guidance system around a pre-calculated tape containing punched holes. This tape was the result of extensive ballistics calculations on the new IBM/Aiken Mark I and provided by the mathematical subgroup of the structure unit. Fed into a complicated system of accelerometers and gyroscopes, the guidance section of the rocket “read” the punched tape, on which was encoded the appropriate accelerometer and gyroscope readings for that period in the flight. If the internal readings differed from the pre-loaded tape, mechanical linkages automatically increased or reduced power until the readings again matched those on the pre-loaded tape.
This was far from a perfect solution, as it could not compensate for outside forces, such as variations in high-altitude winds or other unforeseeable problems, but it was available during the war and constituted the core of the guidance system for the Howitzers used in the two attacks that ended the war. Also critical was the need to ensure that the calculations done in Oak Canyon and pre-loaded into the rockets were as accurate as possible. One misplaced variable, one improperly solved equation, and the rockets might land dozens of miles away from their intended target. As it was, Draper’s system promised accuracy only to 10 kilometers — about 7 miles. In the jargon of ballistics, it had a Circular Error Probability (CEP) of 10 km. That meant half the rockets fired at a given target would land outside that 10-kilometer radius. The other half would land inside it.
Draper’s first test of this new inertial navigation system took place in May 1944 aboard a B-29 flying from Los Angeles to Boston. The bomber had shades drawn over all of its windows, and its sole means of navigation was through the complicated 3,700-pound assembly of containers and crates in the belly of the aircraft. With Draper and two assistants aboard, the aircraft managed to navigate across the entire United States, missing its target by only 4 miles. As successful as that might sound, the aircraft was traveling at less than 2 percent of the speed of one of the Howitzers, and on a far simpler trajectory. Despite his disappointment, Draper set about improving the system for use in the Howitzers.
The temperature of the exhaust is 'easily' measured, and they know what the melting points of the various metals are. Why should they have to test them in engines to tell that there's a problem? That's something that's 'easy' to test ahead of time.In Oak Canyon, other efforts were aimed at improving the rockets’ ability to respond to commands given by the navigation system. The A-series rocket and the first iterations of the Rifle used control vanes for steering. These, when pushed into the stream of rocket exhaust, deflected some of the exhaust, thus steering the rocket. This was an effective solution but less than ideal for a few reasons. First and foremost, because the rocket lost up to 2 percent of its thrust when the vanes were dipped into the exhaust. This reduced the rocket’s payload capacity, apogee (top altitude) and range. Second, the vanes had the disturbing tendency to disintegrate under the extreme heat of the rocket exhaust. With short-range rockets and those using fuels that burned at a cooler temperature, this problem wasn’t as severe. But as the R-2 engines attained longer and longer burn times, the problem of disintegrating vanes became worse and worse. Even alloys of molybdenum, chromium, and other expensive heat-resistant metals only withstood the exhaust for a short time before simply melting and falling apart.
In February 1944, things reached a breaking point. In tests of the newest engine, the R-3, which produced thrust of more than 150,000 pounds and temperatures of more than 5,800 degrees Fahrenheit, no control vane lasted for more than 45 seconds of the 150-second burn time required.
Errr... Gimballing engines works fine for liquid rockets. Your paper-tape guidance system might, MIGHT work for liquids. Solids? Don't see how.By that point, the majority of the Howitzers’ major components were either under development or merely needed to be refined for final use. Engines powerful enough to lift the Howitzer had been developed, as had a system to guide it, to provide its fuel, and to support its structure. Despite those successes, much work remained. Fuel types continued to be developed and refined. In Henderson, Russian-born William Lemkin improved the efficiency of DuPont’s solid-fueled engines by suggesting an audacious mixture using far more aluminum powder than had been proposed by Frank Malina, the fuel’s inventor. The final formula: 70 percent ammonium perchlorate, 16 percent aluminum powder, 12 percent polybutadiene, 1.8 percent solidifying epoxy and 0.2 percent iron oxide, wasn’t created until February 1945, well after the first batches of fuel started to roll out of the chemical plants in Nevada.
http://www.centennialofflight.gov/essay/Evolution_of_Technology/reentry/Tech19.htmAnother critical development that took place during the late 1944 period was the revelation that the appropriate nosecone shape for the Howitzers wasn’t a clean, streamlined needlepoint. It was a blunt end. The reason for this was one of heat and friction. A sharp-edged object re-entering the atmosphere would create enormous friction as it screamed toward the Earth’s surface at a high rate of speed. Even the most heat-resistant materials would burn up, causing the warhead to explode well before reaching the ground. As determined by H. Julian Allen, Caltech’s Qian Xuesen and Columbia’s Karl Cohen, a blunt-nosed warhead would cause air to pile up in front of it as it entered the atmosphere. It would be moving faster than air could get out of its way, and the resulting compressed shock wave would act as an insulator, receiving the first impact of the undisturbed air in front of the re-entering warhead. Despite this effect, massive amounts of energy would still be transmitted to the warhead, and a heat sink and heat shield became a top priority.
High-heat TNT? ?? cites?To reduce the amount of shielding needed, a special temperature-resistant version of TNT was developed for use in the Howitzers. This explosive was far less prone to spontaneous detonation when exposed to high heat and came to be used in other engineering and technical areas where that characteristic was useful. Nevertheless, a heat shield was needed. The first theories were that a solid copper heat shield might be appropriate. Copper is an excellent conductor, and backed with a ceramic insulator, it might have proved an effective shield. However, because of the military need for copper to produce brass for ammunition, this idea was discarded at an early stage. Harry Julian Allen, formerly of NACA’s theoretical aerodynamics branch, instead suggested a layered fiberglass/asbestos heat shield with steel stiffeners. Fiberglass was still a relatively new material, but its characteristics — it begins to degrade at more than 3,600 degrees Fahrenheit — made it workable for an ablative heat shield. In an ablative heat shield, portions of the heat shield erode as the spacecraft re-enters the atmosphere, removing heat from the object at the cost of some of its protection. This approach was what ultimately was used in the Howitzers’ warheads, though it, too, was quickly replaced for better materials after the war’s conclusion.
Holy Cow! I was going to question a successful bowel resection that early, but there's a case dating back to like 1897 (I closed the window, so I might have the exact year wrong). OK. (Peritonitis is really, really, REALLY a problem. Penicillin is new and they hardly know how to use it. still, obviously possible.)The same month that Goddard’s cancer was discovered, von Karman was also diagnosed with cancer. His was an intestinal cancer, and thanks to excellent treatment by doctors specially assigned to his case, he was able to make a full recovery two months after surgery removed three feet of intestine. A less-skilled surgeon might have caused complications from the procedure, which was not as common in 1944 as it is today, but von Karman was granted special treatment because of his position as head of the Manhattan Project’s scientific contingent.
Err... no. Alumin(i)um has a density of 2.7, Titanium 4.5. Titanium is only marginally lighter than steel, actually.
Is the paper tape idea yours? or did someone else come up with it
As for vacuum tubes not standing up - they put entire radar sets into SHELLS (which is what a proximity fuze is). So, by late in the war, you have SOME chance for a very rugged vacuum tube computer (which would also be very expensive, of course).
The temperature of the exhaust is 'easily' measured, and they know what the melting points of the various metals are. Why should they have to test them in engines to tell that there's a problem? That's something that's 'easy' to test ahead of time.
Solids? Don't see how.
Also, did they HAVE sufficiently high-speed wind tunnels to test for the problems in 1944?
High-heat TNT? ?? cites?
Right, I just doubt that they can get it 'pre-set' enough. YMMV. I can't imagine adjustments for solids working, because you'd surely need to throttle the engines up and down a touch to adjust for side deviations. I THINK paper tape control for solids is ASB. Paper tape for liquids is - well, I don't think it'd work, but I'm not a rocket engineer.It was used in different applications before the war and afterward, though not in missile guidance systems. It was used in areas where machines or devices needed to perform pre-set functions.
rightUnfortunately, as you stated, asking such a computer to do derivations from the recordings of an accelerometer and gyroscopes is a bit much for the wartime period. They'll be used in the missiles' proximity fuses and another secondary terminal radar guidance system which will be introduced in a later segment.
Ummm... but look at the temperature of the burning fuelThough they know the capabilities of individual components, they do not know the capability of the entire assembly, whether some manufacturing stage might have introduced a defect, whether a component might have adverse effects on others, whether the brazing and welding might have weakened the structure ... and so on.
http://astronautix.com/props/loxosene.htm said:Temperature of Combustion: 3,670 deg K.
vshttp://astronautix.com/props/loxlh2.htm said:Temperature of Combustion: 2,985 deg K
http://en.wikipedia.org/wiki/Molybdenum said:
http://en.wikipedia.org/wiki/Niobium said:
http://en.wikipedia.org/wiki/Tantalum said:
Ah, forgot that. Ja, probably possible.In a previous update, I mentioned the introduction of shock tubes, which are necessary for high-speed, high-temperature testing. This was done in early 1943, which allows for more than a full year of around-the-clock experimentation before the blunt bodies theory is developed. OTL, it was determined in 1951 despite a lack of funding for rockets.
Oh... You meant High Explosive, not TNT. Ja, sure, fine. TNT is NOT a generic for 'High Explosive', it is Trinitrotoluene (I think I got the spelling correct). I didn't see how much you could fiddle with a single chemical.Whether simple RDX (which was available and had a higher detonation point than TNT) would do, I'm not sure because I don't know what temperatures could be expected.
It's not a matter of structure, the vanes themselves are guaranteed to melt.
Astronautix doesn't list Isp for the engines we want to look at, but looking at the graph at the top of http://astronautix.com/props/solid.htm it looks like Isp on the early solids was a lot lower, which would suggest rather cooler temperatures. For that matter, how do they keep Shuttle SRBs from burning through their cases? Hmmm....?And yet the Pershing missile and other first-generation solid fueled missiles use them. ...
Edit: I see the problem; we were looking at the temperature of the liquid-fueled rocket exhaust and comparing it to the solid-fueled rocket steering vanes.