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Andrew Higgins wrote
The maximum muzzle velocity of the 1960's era HARP gun never exceeded 2 km/s. My bad. The figure I gave was a projection, and wasn't actually achieved. However, I've seen several ref's to a 2.3 km/s shot, from the Canadian guy who wrote a paper on the HARP in about 1966. Whether that was actually shot or not, I don't know. There are a few 13,000 fps (~4km/s) powder guns around today, and I've heard of plans for a 5km/s one Reference, please. Working on it. The 5 kps gun is more likely to yield results, I know some guys involved. I've a feeling the 4 kps one is too classified. You can prove on gasdynamics grounds that a powder gun can *never* exceed 3 km/s muzzle velocity. The "gas speed" limit in a "gun" is not the speed of sound in the gas, assuming no projectile. Ignoring for the moment wall effects, the mass of gas in the "barrel" can be bulk accelerated to some velocity by pressure from behind - and a _very light_ projectile can then be accelerated to the speed of sound relative to the travelling mass of gas, by it's expansion. Which is more than the speed of sound relative to the breech. Of course, it's far more complex than that. ![]() Experimental railguns have already achieved 30,000+ fps, well over orbital velocity, References, please. I am not aware of any railguns exceeding 6 km/s. The 30,000 fps plus figure came from a USN press report, with no details. I think it slipped out. I don't know if it's right, but for sure some research and development on railguns is classified. The same is even more true of travelling charge guns (which, btw, the 5 kps gun is not). However, these guys reportedly got 7.1 km/s: http://www.ioffe.rssi.ru/PAPERS/94w06.pdf and a railgun at ISAS (in Japan) gets 7+ km/s too, or so they've said, but they are a bit reticent. They are also working on a 10 kps+ shaped-charge "thrower". I have the impression that considerable unannounced progress has been made. This looks interesting: http://library.kmitnb.ac.th/df/ieee40/370192.pdf By the way, does anyone know anything about an "electric gun" at LLNL? Not a railgun, I'd guess, they were talking about 15-18 kps? -- Peter Fairbrother |
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How about a series of superguns of different sizes? You start with a small gun,
it fires a projectile that hits an object hovering in front of it. The projectile knocks the object forward and in front of a second slightly larger gun which fires a projectile hitting. The target goes faster and higher each time it is hit by projectiles fired by increasingly larger superguns. The guns are igged to fire at a precisely timed moment hitting the target as it passes in front of it. The projectiles never have a fast enough relative velocity to actually destroy the target, only to push it faster and higher. Eventually you need superguns to push the target to near orbital velocities. Each supergun only fires once for the launch of the payload. Does this sound like a good idea? Tom |
#34
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Peter Fairbrother wrote in message ...
Andrew Higgins wrote You can prove on gasdynamics grounds that a powder gun can *never* exceed 3 km/s muzzle velocity. The "gas speed" limit in a "gun" is not the speed of sound in the gas, assuming no projectile. Correct: maximum velocity is *not* equal sound speed in propellant gas, but they *are* directly related. In fact, as can be shown from the Method of Characteristics for unsteady gasdynamics, the maximum velocity of a gas expansion is: Vmax = 2 a0/(g-1) ....where "g" is the ratio of specific heats and a0 is the *initial* speed of sound of the propellant. For g = 1.4, for example, Vmax = 5 a0. This is for a complete expansion to vacuum, only realizable with a zero mass projectile. In practice, actual guns get nowhere near this limit. The base pressure drops off exponentially as the projectile accelerates, approximately as: p/p0 ~ exp(-g * V/a0) ....where p0 is the initial pressure (before projectile started moving). Once the projectile has reached twice a0, the base pressure is only about 5% its initial value, and guns can rarely accelerate projectiles any faster than this. For powder guns, the gaseous propellant is the combustion products of the powder, which typically have an initial sound speed around 1 km/s. Hence, the speed limit of about 2 km/s for powder guns. I am very skeptical of claims of a 3+ km/s powder gun. Experimental railguns have already achieved 30,000+ fps, well over orbital velocity, References, please. I am not aware of any railguns exceeding 6 km/s. The 30,000 fps plus figure came from a USN press report, with no details. I think it slipped out. I don't know if it's right, but for sure some research and development on railguns is classified. The same is even more true of travelling charge guns (which, btw, the 5 kps gun is not). Traveling charge guns, as far as I am aware, have *never* demonstrated a boost in muzzle velocity over conventional, breech-fed guns. The last review I've seen was: Baer, P.G., and I.W. May, "Traveling-Charge Effect" in "Gun Propulsion Technology" ed. L. Stiefel, Vol 109, AIAA Progress in Astronautics and Aeronautics, 1988, pp. 499-536. ....and I am not aware of any new experimental results since then. However, these guys reportedly got 7.1 km/s: http://www.ioffe.rssi.ru/PAPERS/94w06.pdf Thanks for the reference; this claim, if true, would be a new velocity record for a rail gun. However, I would need to see more data from the actual test before being convinced; some claims at record muzzle velocities from rail guns have actually been jets of plasma squirting from the end of the rails, not coherent projectiles. I have the impression that considerable unannounced progress has been made. This looks interesting: http://library.kmitnb.ac.th/df/ieee40/370192.pdf I think "Promising but unconfirmed theoretical study" is more appropriate description of this paper, rather than "considerable unannounced progress." By the way, does anyone know anything about an "electric gun" at LLNL? Not a railgun, I'd guess, they were talking about 15-18 kps? I am not aware of a 15-18 km/s gun at LLNL, although certain there is interest there (an elsewhere) in such a device. You may be thinking of two different, recent developments: One is the use of the Sandia Z machine (basically, a very, very large pulsed power supply) to launch thin metal foils to velocities of 15-20 km/s via magnetic loading: http://www.sandia.gov/media/NewsRel/NR2001/flyer.htm The other is a 3-stage gun at Sandia that has also accelerated small flyer plates ( 1g) to 15 km/s: http://www.cs.sandia.gov/HPCCIT/hyprvel.html Note that the third stage of this 3-stage gun is basically the 2nd-stage projectile impacting a special, density-gradient material that "smoothly" shocks the smaller flyer to the final velocity. In both of these devices, there are still concerns if the projectile is actually intact, or has been "spalled" by the acceleration process. Note that all of this work uses projectiles smaller than 1 g, and is used exclusively for fundamental equation of state studies motivated by inertial confinement fusion studies, H-bomb physics, and fundamental planetary physics. Other than as a possible simulator for micrometeoroid and orbital debris impact, these devices have no relevance to the subject of this thread ("Cheaper way to space!? A supergun.") because they cannot scale and because they violently shock their projectiles to their yield strength. As for concepts that are scalable for "soft" direct space launch, the two most interesting concepts (the Ram Accelerator and, more speculatively, the Slingatron) remain too underdeveloped to make definitively assessments of feasibility. Neither of these concepts have ever had the funding support necessary to determine what the maximum velocities achievable are, although a small amount of basic research is continuing on both. -- Andrew J. Higgins Mechanical Engineering Dept. Assistant Professor McGill University Shock Wave Physics Group Montreal, Quebec CANADA http://www.mcgill.ca/mecheng/staff/academic/higgins/ |
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Peter Fairbrother wrote in message ...
Andrew Higgins wrote You can prove on gasdynamics grounds that a powder gun can *never* exceed 3 km/s muzzle velocity. The "gas speed" limit in a "gun" is not the speed of sound in the gas, assuming no projectile. Correct: maximum velocity is *not* equal sound speed in propellant gas, but they *are* directly related. In fact, as can be shown from the Method of Characteristics for unsteady gasdynamics, the maximum velocity of a gas expansion is: Vmax = 2 a0/(g-1) ....where "g" is the ratio of specific heats and a0 is the *initial* speed of sound of the propellant. For g = 1.4, for example, Vmax = 5 a0. This is for a complete expansion to vacuum, only realizable with a zero mass projectile. In practice, actual guns get nowhere near this limit. The base pressure drops off exponentially as the projectile accelerates, approximately as: p/p0 ~ exp(-g * V/a0) ....where p0 is the initial pressure (before projectile started moving). Once the projectile has reached twice a0, the base pressure is only about 5% its initial value, and guns can rarely accelerate projectiles any faster than this. For powder guns, the gaseous propellant is the combustion products of the powder, which typically have an initial sound speed around 1 km/s. Hence, the speed limit of about 2 km/s for powder guns. I am very skeptical of claims of a 3+ km/s powder gun. Experimental railguns have already achieved 30,000+ fps, well over orbital velocity, References, please. I am not aware of any railguns exceeding 6 km/s. The 30,000 fps plus figure came from a USN press report, with no details. I think it slipped out. I don't know if it's right, but for sure some research and development on railguns is classified. The same is even more true of travelling charge guns (which, btw, the 5 kps gun is not). Traveling charge guns, as far as I am aware, have *never* demonstrated a boost in muzzle velocity over conventional, breech-fed guns. The last review I've seen was: Baer, P.G., and I.W. May, "Traveling-Charge Effect" in "Gun Propulsion Technology" ed. L. Stiefel, Vol 109, AIAA Progress in Astronautics and Aeronautics, 1988, pp. 499-536. ....and I am not aware of any new experimental results since then. However, these guys reportedly got 7.1 km/s: http://www.ioffe.rssi.ru/PAPERS/94w06.pdf Thanks for the reference; this claim, if true, would be a new velocity record for a rail gun. However, I would need to see more data from the actual test before being convinced; some claims at record muzzle velocities from rail guns have actually been jets of plasma squirting from the end of the rails, not coherent projectiles. I have the impression that considerable unannounced progress has been made. This looks interesting: http://library.kmitnb.ac.th/df/ieee40/370192.pdf I think "Promising but unconfirmed theoretical study" is more appropriate description of this paper, rather than "considerable unannounced progress." By the way, does anyone know anything about an "electric gun" at LLNL? Not a railgun, I'd guess, they were talking about 15-18 kps? I am not aware of a 15-18 km/s gun at LLNL, although certain there is interest there (an elsewhere) in such a device. You may be thinking of two different, recent developments: One is the use of the Sandia Z machine (basically, a very, very large pulsed power supply) to launch thin metal foils to velocities of 15-20 km/s via magnetic loading: http://www.sandia.gov/media/NewsRel/NR2001/flyer.htm The other is a 3-stage gun at Sandia that has also accelerated small flyer plates ( 1g) to 15 km/s: http://www.cs.sandia.gov/HPCCIT/hyprvel.html Note that the third stage of this 3-stage gun is basically the 2nd-stage projectile impacting a special, density-gradient material that "smoothly" shocks the smaller flyer to the final velocity. In both of these devices, there are still concerns if the projectile is actually intact, or has been "spalled" by the acceleration process. Note that all of this work uses projectiles smaller than 1 g, and is used exclusively for fundamental equation of state studies motivated by inertial confinement fusion studies, H-bomb physics, and fundamental planetary physics. Other than as a possible simulator for micrometeoroid and orbital debris impact, these devices have no relevance to the subject of this thread ("Cheaper way to space!? A supergun.") because they cannot scale and because they violently shock their projectiles to their yield strength. As for concepts that are scalable for "soft" direct space launch, the two most interesting concepts (the Ram Accelerator and, more speculatively, the Slingatron) remain too underdeveloped to make definitively assessments of feasibility. Neither of these concepts have ever had the funding support necessary to determine what the maximum velocities achievable are, although a small amount of basic research is continuing on both. -- Andrew J. Higgins Mechanical Engineering Dept. Assistant Professor McGill University Shock Wave Physics Group Montreal, Quebec CANADA http://www.mcgill.ca/mecheng/staff/academic/higgins/ |
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Peter Fairbrother wrote in message ...
Andrew Higgins wrote You can prove on gasdynamics grounds that a powder gun can *never* exceed 3 km/s muzzle velocity. The "gas speed" limit in a "gun" is not the speed of sound in the gas, assuming no projectile. Correct: maximum velocity is *not* equal sound speed in propellant gas, but they *are* directly related. In fact, as can be shown from the Method of Characteristics for unsteady gasdynamics, the maximum velocity of a gas expansion is: Vmax = 2 a0/(g-1) ....where "g" is the ratio of specific heats and a0 is the *initial* speed of sound of the propellant. For g = 1.4, for example, Vmax = 5 a0. This is for a complete expansion to vacuum, only realizable with a zero mass projectile. In practice, actual guns get nowhere near this limit. The base pressure drops off exponentially as the projectile accelerates, approximately as: p/p0 ~ exp(-g * V/a0) ....where p0 is the initial pressure (before projectile started moving). Once the projectile has reached twice a0, the base pressure is only about 5% its initial value, and guns can rarely accelerate projectiles any faster than this. For powder guns, the gaseous propellant is the combustion products of the powder, which typically have an initial sound speed around 1 km/s. Hence, the speed limit of about 2 km/s for powder guns. I am very skeptical of claims of a 3+ km/s powder gun. Experimental railguns have already achieved 30,000+ fps, well over orbital velocity, References, please. I am not aware of any railguns exceeding 6 km/s. The 30,000 fps plus figure came from a USN press report, with no details. I think it slipped out. I don't know if it's right, but for sure some research and development on railguns is classified. The same is even more true of travelling charge guns (which, btw, the 5 kps gun is not). Traveling charge guns, as far as I am aware, have *never* demonstrated a boost in muzzle velocity over conventional, breech-fed guns. The last review I've seen was: Baer, P.G., and I.W. May, "Traveling-Charge Effect" in "Gun Propulsion Technology" ed. L. Stiefel, Vol 109, AIAA Progress in Astronautics and Aeronautics, 1988, pp. 499-536. ....and I am not aware of any new experimental results since then. However, these guys reportedly got 7.1 km/s: http://www.ioffe.rssi.ru/PAPERS/94w06.pdf Thanks for the reference; this claim, if true, would be a new velocity record for a rail gun. However, I would need to see more data from the actual test before being convinced; some claims at record muzzle velocities from rail guns have actually been jets of plasma squirting from the end of the rails, not coherent projectiles. I have the impression that considerable unannounced progress has been made. This looks interesting: http://library.kmitnb.ac.th/df/ieee40/370192.pdf I think "Promising but unconfirmed theoretical study" is more appropriate description of this paper, rather than "considerable unannounced progress." By the way, does anyone know anything about an "electric gun" at LLNL? Not a railgun, I'd guess, they were talking about 15-18 kps? I am not aware of a 15-18 km/s gun at LLNL, although certain there is interest there (an elsewhere) in such a device. You may be thinking of two different, recent developments: One is the use of the Sandia Z machine (basically, a very, very large pulsed power supply) to launch thin metal foils to velocities of 15-20 km/s via magnetic loading: http://www.sandia.gov/media/NewsRel/NR2001/flyer.htm The other is a 3-stage gun at Sandia that has also accelerated small flyer plates ( 1g) to 15 km/s: http://www.cs.sandia.gov/HPCCIT/hyprvel.html Note that the third stage of this 3-stage gun is basically the 2nd-stage projectile impacting a special, density-gradient material that "smoothly" shocks the smaller flyer to the final velocity. In both of these devices, there are still concerns if the projectile is actually intact, or has been "spalled" by the acceleration process. Note that all of this work uses projectiles smaller than 1 g, and is used exclusively for fundamental equation of state studies motivated by inertial confinement fusion studies, H-bomb physics, and fundamental planetary physics. Other than as a possible simulator for micrometeoroid and orbital debris impact, these devices have no relevance to the subject of this thread ("Cheaper way to space!? A supergun.") because they cannot scale and because they violently shock their projectiles to their yield strength. As for concepts that are scalable for "soft" direct space launch, the two most interesting concepts (the Ram Accelerator and, more speculatively, the Slingatron) remain too underdeveloped to make definitively assessments of feasibility. Neither of these concepts have ever had the funding support necessary to determine what the maximum velocities achievable are, although a small amount of basic research is continuing on both. -- Andrew J. Higgins Mechanical Engineering Dept. Assistant Professor McGill University Shock Wave Physics Group Montreal, Quebec CANADA http://www.mcgill.ca/mecheng/staff/academic/higgins/ |
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Peter Fairbrother wrote in message ...
and a railgun at ISAS (in Japan) gets 7+ km/s too, or so they've said, but they are a bit reticent. They are also working on a 10 kps+ shaped-charge "thrower". Shaped charge explosives capable of producing 10+ km/s metallic jets have been around since the Second World War. In fact, Fritz Zwicky can lay claim (albeit tenuous) to having launched the first artificial object into solar orbit in 1957 (just 12 days after Sputnik 1) by using a Aerobee rocket to launch a shaped charge to high altitude, then detonating the explosive to send out jets at 15 km/s. Similar work was also done by Zwicky and Fred Whipple in 1946, using captured V-2's. You can read more about this fascinating story he http://utenti.lycos.it/paoloulivi/aerobee.html http://www.slac.stanford.edu/pubs/be...1-1-maurer.pdf http://www.ufx.org/gfb/zwickoralhist.htm http://www.ufx.org/gfb/artifmet.htm -- Andrew J. Higgins Mechanical Engineering Dept. Assistant Professor McGill University Shock Wave Physics Group Montreal, Quebec CANADA http://www.mcgill.ca/mecheng/staff/academic/higgins/ |
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Andrew Higgins wrote
However, these guys reportedly got 7.1 km/s: http://www.ioffe.rssi.ru/PAPERS/94w06.pdf Thanks for the reference; this claim, if true, would be a new velocity record for a rail gun. However, I would need to see more data from the actual test before being convinced; some claims at record muzzle velocities from rail guns have actually been jets of plasma squirting from the end of the rails, not coherent projectiles. http://ieeexplore.ieee.org:80/xpl/ab...rod=JNL&arnumb er=195613&arSt=431&ared=434&arAuthor=Kawashima%2C+ N.%3B+Yamori%2C+A.%3B+Yana gisawa%2C+M.%3B+Kubo%2C+H.%3B+Kohno%2C+M.%3B+Teii% 2C+S.&arNumber=195613&a_id 0=195609&a_id1=195610&a_id2=195611&a_id3=195612&a_ id4=195613&a_id5=195614&a_ id6=195615&a_id7=195616&a_id8=195617&a_id9=195618& a_id10=195619&a_id11=19562 0&a_id12=195621&a_id13=195622&a_id14=195623&count= 15 reports 7.45 km/s max, and always 6+ kps, again quite a few years ago. There's a figure at http://www.ted.isas.ac.jp/spc/railgun/railgun.html that gives ~7.8 km/s max, but I don't know if it's actual shots or projected results - it looks like shots, but I don't read Japanese. Anyone? Thanks for the Sandia ref's. The guys were working at LLNL tho', so I'm unsure whether they meant the Sandia stuff or something else, I'll ask. BTW, the 10 km/s+ shaped-charge "thrower" isn't from ISAS as I said, but NAL/Mitsubishi. I don't know if it's much more than a design study. -- Peter Fairbrother |
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