CN101839672A - Ultra-high-speed gram-magnitude spherical projectile transmitting device - Google Patents
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Abstract
The invention discloses an ultra-high-speed gram-magnitude spherical projectile transmitting device comprising a two-stage light gas-gun, an extension section and a three-stage accelerating cavity, wherein one end of the extension section is fixedly connected with an outlet of the two-stage light gas-gun, the other end of the extension section is fixedly connected with the connection end of the three-stage accelerating cavity, the three-stage accelerating cavity is designed with a two-section inner diameter, an annular PC resin sleeve is arranged on an annular boss in the cavity towards the extension section, and a high explosive is embedded into the PC resin sleeve; an accelerating unit transmitted by the two-stage light gas-gun comprises a projectile holder, spherical projectiles and annular steel sheets, wherein the projectile holder is in a cylindrical structure, the top of the cylindrical structure is provided with a cylindrical projective end, the annular steel sheets are in sleeve joint with the projective end and are bonded on the front end surface of the projectile holder, and the spherical projectiles are bonded at the projective end of the projectile holder. The ultra-high-speed gram-magnitude spherical projectile transmitting device not only can accelerate gram-magnitude spherical projectiles to 10km/s, but also can ensure that the spherical projectiles are not overheated, has the last length to diameter ratio L/d near 1 and has no primary flyer fragments to follow in order to ensure the effects of space fragment protective structure optimization design and performance evaluation impact test.
Description
Technical field
The present invention relates to a kind of ultra-high-speed gram-magnitude spherical projectile transmitting device.
Background technology
The protection of space debris structure is the key factor that guarantees in rail spacecraft safety.And the design hypervelocity launcher then is the crucial ground experimental technique of protection of space debris Optimal Structure Designing and Performance Evaluation.According to the content of the 4th page of American National aviation in 2003 and space travel office (NASA) report " TP-2003-210788 ", at the 400km height, 51.6 ° of inclination angles, space junk to the relative stroke speed of spacecraft from 1km/s to 15km/s, average 8～9km/s.This just needs the spacecraft safeguard structure to withstand the bump of gram magnitude speed 10km/s fragment.Setting up gram-magnitude spherical projectile 10km/s emitter, is the standard platform of safeguard structure performance test.
In existing emitter, traditional light-gas gun (Light Gas Gun) promotes the bullet motion by Compressed Gas, because the restriction of escape of gas speed, the bullet that generally will restrain magnitude accelerates in the 7km/s, and for lighter bullet, according to the content of the 615th page of periodical " International Journal of ImpactEngineering " the 33rd volume in 2006, three grades of light-gas guns (Three-Stage Light Gas Gun) device of University of Dayton ResearchInstitute (UDRI) design of the U.S. can accelerate to 8.65km/s with the aluminium ball below the diameter 3mm.Because space junk can reach more than the 10km/s the relative stroke speed of spacecraft, so the light-gas gun emitter that promotes based on Compressed Gas can not satisfy the requirement that evaluates and optimizes the protection of space debris structure fully.
In order to obtain the hypervelocity launcher of 10km/s, many schemes have been arranged also on the present disclosed document.In the 16th page of U.S. NASA in 2003 report " TP-2003-210788 ", two kinds of hypervelocity launchers that NASA uses have at present been introduced, three grades of hypervelocity launchers of U.S. Sandia National Laboratory and Inhibited Shaped Charge Launcher (ISCL) emitter of U.S. Southwest Research Institute.The hypervelocity launcher of use impedance gradient film flying (Pillow film flying) actuation techniques of the U.S. Sandia National Laboratory design of introducing in the 799th～811 page of periodical " International Journal of Impact Engineering " the 33rd volume in 2006 wherein, utilizing two-stage light gas gun emission initial velocity is that the Pillow film flying of 6～7km/s drives secondary film flying as elementary film flying.According to the content of 802 pages in this periodical, this device can be that the quality of 9.96mm is the ZrO of 0.934g for the 1.98mm diameter with thickness
2Thin film flying accelerates to 11.7km/s, and is that the quality of 27.00mm is the Al of 2.444g with thickness for the 1.09mm diameter
2O
3Thin film flying accelerates to 14.6km/s.For the Ti6Al4V film flying of the littler 0.03g of quality, this device more can accelerate to it high speed of 19km/s.Because the surge platform in this device in the secondary film flying is narrower, if the excessive film flying of the thickness of film flying will be subjected to the sparse influence in shock wave border so, in film flying, produce big negative pressure, thereby the slabbing phenomenon appears, so can see, this device can only quicken thin film flying, and tests based on the ultrahigh speed penetration of laminar secondary film flying, will underestimate the barrier propterty of structure.Subject matter that this device exists be since directly with secondary film flying from 0 high speed that accelerates to more than the 10km/s, so the surge peak value in the secondary film flying is very big, cause the impact temperature rise of secondary film flying higher, the target effect is hit in influence; Thin simultaneously film flying is subjected to the aerial statue after the thump emission also to be difficult to guarantee, the hitting the target experiment and will have uncertainty of the film flying of so same speed.And the panus behind the secondary film flying of this technology (clashing into secondary film flying by the Pillow film flying produces) will exert an influence to the penertration resistance performance test of safeguard structure.And for second kind of experimental provision ISCL of the current use of U.S. NASA, content according to the 168th～169 page of periodical " International Journal of ImpactEngineering " the 20th volume in 1997, the ISCL hypervelocity launcher can only be 2～3 with draw ratio, quality is that the open column shape aluminium bomb ball of 0.8～1.5g accelerates to 11km/s, this device is to the limitation of bullet shape, and the jet and the distortion of emission final states, also limited its application in protection of space debris Optimal Structure Designing and Performance Evaluation.
Except two kinds of hypervelocity launchers of NASA practical application, the imagination that also has other hypervelocity launcher can be with 10 as going up the static dust accelerator of introducing (Electrostatic Dust Accelerators) the 1417th～1418 page of the 28th the 9th phase of volume of calendar year 2001 periodical " Advances in Space Research "
-15～10
-9The dust of g accelerates to 60km/s; Plasma accelerator (Plasma Accelerators) can be with 10
-8～10
-4The dust of g accelerates to 20km/s.Certainly the problem of these two kinds of hypervelocity launchers is that the object quality of quickening is too light, can not reach the requirement of protection of space debris Optimal Structure Designing and Performance Evaluation.And roll up the electric blasting device (Electric Gun) of the 3rd phase the 369th～374 page of introduction in June, 2006 periodical " Experimental Mechanics " the 21st, utilize metal bridge paper tinsel discharge-induced explosion to produce high-density plasma and expansion rapidly, driving the thin film flying high-speed motion of insulation can be 10mm with diameter, and thickness is that the Mylar film film flying of 0.1mm accelerates to 10km/s.Yet the same with the hypervelocity launcher that uses impedance gradient film flying actuation techniques, the film flying that this device quickens is too thin, can not satisfy the requirement of protection of space debris Optimal Structure Designing and Performance Evaluation.And, in the process of quickening, also be attended by the problem of ablation because this device utilizes high-density plasma to quicken.
Summary of the invention
Technical problem to be solved by this invention provides a kind of ultra-high-speed gram-magnitude spherical projectile transmitting device, this device not only can quicken gram-magnitude spherical projectile to 10km/s, and the temperature rise that can guarantee bullet is unlikely too high, the distortion limited (draw ratio L/d near 1 class sphere) of emission final states, and there is not the follow-up of elementary film flying fragment, with the effect of the bump test that guarantees protection of space debris Optimal Structure Designing and Performance Evaluation.
The present invention addresses the above problem the technical scheme that is adopted: ultra-high-speed gram-magnitude spherical projectile transmitting device, comprise two-stage light gas gun, extension, three grades of accelerating cavities, described extension one end is fixedlyed connected with the outlet of two-stage light gas gun, the other end is fixedlyed connected with the link of three grades of accelerating cavities, described three grades of accelerating cavities are that the link internal diameter is greater than gauge structure in the two-period form of other end internal diameter, ledge structure ringwise and ring-shaped step structure place than the junction of large diameter and less internal diameter are provided with ring-shaped P C resin cover, and PC resin cover is embedded in and is provided with high explosive; The accelerator module of described two-stage light gas gun emission comprises bullet holder, cannonball and annular steel disc, the bullet holder is that cylindrical structure and cylinder end face have cylindrical protruding end, the annular steel disc is socketed on the protruding end and sticks in the front end face of bullet holder, cannonball sticks in the protruding end of bullet holder, and described annular steel disc and PC resin cover are complementary.
The tapered structure of the front end of described annular steel disc, the detonation mode that makes annular steel disc bump high explosive are detonated simultaneously from the whole explosive end face of plane impact and have been become annular line and detonate, and have reduced the center behind the explosive initiation and have converged.The shaped design of this annular steel disc changes detonation mode, has reduced the influence of central jet.
Fixedly connected by connecting flange with two-stage light gas gun in described extension.
Fixedly connected by three grades of chamber flanges with three grades of accelerating cavities in described extension.
Also comprise and be socketed on the outer protection sleeve of three grades of chamber flanges.
Described protruding end end has the hemisphere face groove, and cannonball places in the hemisphere face groove.
Described high explosive detonates behind cannonball, thereby forms the motive force that cannonball is quickened behind cannonball.
After described cannonball was quickened for the first time by two-stage light gas gun, the high explosive of being ignited by annular steel disc bump in three grades of accelerating cavities quickened once more.With the existing different type of drive of multistage driving, the present invention adopts gas-powered to same bullet and changes the two-stage drive of quick-fried driving, and the elementary film flying that is different from existing multistage driving drives secondary film flying.
In sum, the invention has the beneficial effects as follows:
1 the present invention use two-stage light gas gun with the holder of Merlon (PC) resin bullet with and ring-type steel film flying that go up to settle and cannonball (the being accelerator module) speed that steadily accelerates to 6-7km/s, then utilize the high explosive of placing in three grades of accelerating cavities of annular steel disc bump of settling in the holder of PC resin bullet, explosive detonation produces high pressure makes resin be dissociated into gas, the gas that disassociation generates is formed gases at high pressure together with detonation product, impact the ultrahigh speed of ACCELERATING PROJECTILE to 10km/s, the temperature rise that can guarantee bullet is unlikely too high, last draw ratio L/d is near 1, and there is not the follow-up of elementary film flying fragment, with the effect of the bump test that guarantees protection of space debris Optimal Structure Designing and Performance Evaluation.
2, creativeness of the present invention is, on the two-stage light gas gun platform, the secondary formula drives the speed of cannonball to 10km/s; The resin that three grades of interior high explosives of accelerating cavity promptly impact behind the disassociation bullet produces gases at high pressure, has kept the high voltage platform that advances bullet again.External three grades of traditional big gun technology, the film flying bump thin slice bullet that only utilizes the two-stage light gas gun emission is to produce ultrahigh speed.
Description of drawings
Fig. 1 is a structural representation of the present invention;
Fig. 2 is the structural representation of protection sleeve of the present invention;
Fig. 3 is the two-dimentional axial symmetry analog result of AUTODYN-2D, and cannonball speed over time when being the gram-magnitude spherical aluminium bomb ball of 6km/s for quickening initial velocity;
Fig. 4 is the two-dimentional axial symmetry analog result of AUTODYN-2D, when being the gram magnitude aluminium bomb ball of 6km/s for quickening initial velocity behind the steel film flying bump explosive through the species distribution situation of 5 μ s, wherein the most dark zone is a cannonball.
Fig. 5 is the two-dimentional axial symmetry analog result of AUTODYN-2D, for quicken initial velocity when being the heavy titanium alloy bullet of the 1.6g of 6km/s behind the steel film flying bump explosive through the species distribution situation of 7 μ s, wherein the most dark zone is a cannonball.
Mark and corresponding parts title in the accompanying drawing: 1-two-stage light gas gun, 2-connecting flange, the holder of 3-bullet, 4-extension, 5-cannonball, 6-annular steel disc, three grades of chamber flanges of 7-, 8-high explosive, 9-PC resin cover, three grades of accelerating cavities of 10-, 11-protection sleeve.
The specific embodiment
Below in conjunction with embodiment and accompanying drawing, to the detailed description further of the present invention's do, but embodiments of the present invention are not limited thereto.
Extremely shown in Figure 5 referring to Fig. 1, ultra-high-speed gram-magnitude spherical projectile transmitting device of the present invention is bonded in cannonball in the hemisphere face groove of Merlon (PC) bullet holder, quicken through two-stage light gas gun, bullet holder and bullet enter the extension with the speed of about 6-7km/s, then steadily enter three grades of accelerating cavities, the PC resin cover of three grades of interior bonding annulars of accelerating cavity, annular groove is embedded in ring plate shape high explosive (JOB 9003), entered the inner chamber of PC resin cover when bullet, No. 45 steel film flyings of bullet holder front end face (being annular steel disc) high-speed impact explosive, produce strong detonation, high-speed jet makes the Merlon disassociation behind the bullet, produce that gases at high pressure impact and further drive cannonball, obtain near or surpass the speed of 10km/s.
Ultra-high-speed gram-magnitude spherical projectile transmitting device of the present invention mainly by the PC resin bullet holder of secondary big gun transmitter section with and go up cannonball and the ring-type steel film flying of settling; The extension of installing behind the secondary big gun, three grades of accelerating cavities, PC resin cover and high explosives, and connecting flange and protection sleeve composition.
As shown in Figure 1, cannonball 5 sticks in the hemisphere face groove of the PC bullet holder 3 middle part sections of stretching out, and simultaneously annular steel film flying 6 is inserted in the section of stretching out of PC bullet holder, and sticks in PC bullet holder 3 front end faces.Annular steel disc 6 and cannonball 5 accelerate to 6-7km/s by two-stage light gas gun 1 together with PC bullet holder 3 and enter extension 4 with and subsequent three grades of accelerating cavities 10.
Link by connecting flange 2 between two-stage light gas gun 1 and the extension 4; extension 4 is then linked by three grades of chamber flanges and protection sleeve 7 with between three grades of accelerating cavities 10; the concrete installation signal of peripheral protection sleeve as shown in Figure 2; wherein extension 4 is used to slow down high temperature gas flow the washing away light-gas gun thorax chamber that ultrahigh speed is impacted generation; 7 safety that are used for further guaranteeing light-gas gun and target chamber of protection sleeve are further protected the destruction to target chamber such as slabbing film flying.
The PC resin cover 9 of three grades of accelerating cavity 10 interior bonding annulars, embed ring-type high explosive 8 in the PC resin cover 9, after annular steel disc 6 and cannonball 5 enter three grades of accelerating cavities 10 together with PC bullet holder 3, because cannonball 5 sticks in the hemisphere face groove of the PC bullet holder 3 middle part sections of stretching out, so the steel film flying 6 that has entered PC bullet holder 3 leading portion faces behind the inner chamber of PC resin cover 9 when cannonball is high-speed impact high explosives 8, produce strong detonation, high-speed jet makes the Merlon disassociation behind the bullet, produce that gases at high pressure impact and further drive cannonball 5, obtain near or surpass the speed of 10km/s.The gases at high pressure that the blast of annular explosive column produces can be widened the pressure platform that drives bullet.
When on the two-stage light gas gun experiment porch, projectile transmitting device being installed, need to carry out according to following steps:
Step 1: use silica gel, the explosive ring entirely is installed in the PC annular cover;
Step 2: use epoxide-resin glue, PC annular cover entirely is installed in three grades of chambeies;
Step 3:, the extension is installed at the two-stage light gas gun target chamber;
Step 4: use the feeler gauge conducting, the axis of regulating extension and gas bore road is to neutrality, fixedly connected flange;
Step 5: one side connects three grades of chambeies in the extension;
Step 6: three grades of chamber flanges and protection sleeve are installed;
Step 7: fixing experiment base on the target chamber platform;
Step 8: on the experiment base, peripheral protection sleeve is installed;
Step 9: on the experiment base, the sample target holder is installed.
This ultrahigh speed bullet emitter mainly by the PC resin bullet holder of secondary big gun transmitter section with and go up cannonball and the ring-type steel film flying of settling; The extension of installing behind the secondary big gun, three grades of accelerating cavities, PC resin cover and high explosives, and connecting flange and protection sleeve composition, PC resin cover or the holder of PC resin bullet also can adopt other high molecular polymers with equal performance to replace, wherein,
The holder of PC resin bullet is used to settle cannonball and ring-type steel film flying (being annular steel disc), and by the two-stage light gas gun emission, makes ring-type steel film flying and cannonball steadily accelerate to the speed of 6-7km/s.Front end has cylindrical protruding end and adhesion has cannonball, the annular steel disc is socketed on the protruding end and sticks in the front end face of bullet holder, high explosive is detonated behind cannonball, gases at high pressure that Merlon produces after impacting and dissociating and detonation product gases at high pressure can be widened the pressure platform behind the driving cannonball, for three grades of acceleration provide thrust.
Cannonball hits target after being used for quickening, and carries out striking experiment.
Ring-type steel film flying is used for bump and ignites high explosive, and self kinetic energy is passed to gases at high pressure, for three grades of acceleration provide thrust.Because the steel film flying is column at three grades of accelerating cavity inner impact high explosives and detonates, the back detonation wave that detonates converges the generation central jet to the center and can produce considerable influence to the stable acceleration of cannonball, so as shown in Figure 1, steel film flying front end has adopted conical design, the detonation mode that makes steel film flying bump high explosive detonates simultaneously from the whole explosive end face of plane impact and has become annular line and detonate, high explosive begins to detonate gradually from initial bump line, having reduced the center behind the explosive initiation converges, after the pressure that explosive detonation is produced can be evenly distributed on ball, help keeping the integrality of cannonball.
The extension is used to slow down ultrahigh speed and impacts high temperature gas flow the washing away light-gas gun thorax chamber that produces.
Three grades of accelerating cavities are used to place PC resin cover and high explosive, and detonate at high explosive, and gases at high pressure form the post-concentration directs pressurized gas, to promote cannonball.
PC resin cover is used to wrap up high explosive, and is positioned over together in three grades of accelerating cavities with high explosive, can guarantee the security of explosive in the device assembling process; Guarantee the flatness that the film flying impact explosive charges is detonated, and the axial symmetry of product jet; Buffering explosive product jet is to the impact failure of bullet.Merlon impacts the gases at high pressure of disassociation back generation can widen the pressure platform that drives bullet.Simultaneously, Low ESR Merlon disassociation energy-absorbing can fully reduce the axial impact pressure that three grades of accelerating cavity steel walls stand.
High explosive is used for producing detonation wave in the back of detonating, and generates detonation product and make the resin disassociation form gases at high pressure to promote cannonball, is main motive force.
Connecting flange is used to connect extension and two-stage light gas gun gun barrel, plays the protection sleeve effect simultaneously.
Protection sleeve is used for further guaranteeing the safety of light-gas gun and target chamber, further protects the destruction to target chamber such as slabbing film flying.
Ultra-high-speed gram-magnitude spherical projectile transmitting device provided by the present invention is used two-stage light gas gun cannonball is steadily accelerated to the speed of 6-7km/s, utilizes three grades of accelerating cavities then, impacts the ultrahigh speed of ACCELERATING PROJECTILE to 10km/s.Load with respect to traditional strong detonation, perhaps three grades of lift-off technologies of impedance gradient film flying, according to shock wave theory:
P＝ρ
oDu
Wherein P is the surge in the bullet, D is a shock velocity, u is a particle rapidity behind the shock wave, when impacting from 6-7km/s, bullet accelerates to 10km/s, its surge peak value P directly impacts 1/3rd of pressure when accelerating to 10km/s, thereby can effectively lower the impact temperature rise, and help keeping the integrality of cannonball.The gases at high pressure that strong detonation produces in view of explosive will be kept the pressure platform of a broad, thereby effectively prevent the sparse destruction that causes in shock wave border in the cannonball.The 10km/s ultra-high-speed gram-magnitude spherical projectile that is produced can effectively be applied to protection of space debris Optimal Structure Designing and Performance Evaluation.
Shown that in Fig. 3, Fig. 4, Fig. 5 the two-dimentional axial symmetry of being undertaken by AUTODYN-2D calculates, wherein Fig. 3 has shown a grammes per square metre aluminium bomb ball speed over time, quickens more evenly as can be seen, has kept the long period finally to have reached near 9.5km/s.If the emission rate of secondary gas big gun is increased to 7km/s, bullet can accelerate to 10.5km/s at least.Fig. 4 has shown behind the steel film flying bump explosive that through the species distribution situation of 5 μ s times, wherein the most dark zone is a cannonball.Can see that bullet still keeps the class sphere, obvious difference be arranged with laminar film flying.And outside influencing greatly according to the central jet that result of calculation is produced by strong detonation the pocket behind ball, all temperature rises are very low in all the other zones, and most of regional temperature rise is lower than 200K.
Shown the acceleration effect of TC4 titanium alloy bullet among Fig. 5, wherein the muzzle velocity of secondary gas big gun is 7km/s, and the titanium alloy bullet of 1.6 grammes per square metres accelerates to 9.7km/s, because titanium alloy yield strength height, the bullet distortion is littler.
As mentioned above, just can realize the present invention preferably.
Claims (7)
1. ultra-high-speed gram-magnitude spherical projectile transmitting device, comprise two-stage light gas gun (1), it is characterized in that, also comprise extension (4), three grades of accelerating cavities (10), described extension (4) one ends are fixedlyed connected with the outlet of two-stage light gas gun (1), the other end is fixedlyed connected with the link of three grades of accelerating cavities (10), described three grades of accelerating cavities (10) are that the link internal diameter is greater than gauge structure in the two-period form of other end internal diameter, ledge structure ringwise and ring-shaped step structure place than the junction of large diameter and less internal diameter are provided with ring-shaped P C resin cover (9), and PC resin cover (9) is embedded in and is provided with high explosive (8); The accelerator module of described two-stage light gas gun (1) emission comprises bullet holder (3), cannonball (5) and annular steel disc (6), bullet holder (3) has cylindrical protruding end for cylindrical structure and cylinder end face, annular steel disc (6) is socketed on the protruding end and sticks in the front end face of bullet holder (3), cannonball (5) sticks in the protruding end of bullet holder (3), and described annular steel disc (6) is complementary with PC resin cover (9).
2. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 1, it is characterized in that, the tapered structure of front end of described annular steel disc (6), the detonation mode that makes annular steel disc (6) bump high explosive (8) detonates simultaneously from the whole explosive end face of plane impact and has become annular line and detonate, and has reduced the center behind the explosive initiation and has converged.
3. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 1 is characterized in that, fixedly connected by connecting flange (2) with two-stage light gas gun (1) described extension (4).
4. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 1 is characterized in that, fixedly connected by three grades of chamber flanges with three grades of accelerating cavities (10) described extension (4).
5. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 4 is characterized in that, also comprises being socketed on the outer protection sleeve (11) of three grades of chamber flanges.
6. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 1 is characterized in that, described protruding end end has the hemisphere face groove, and cannonball (5) places in the hemisphere face groove.
7. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 6 is characterized in that, described high explosive (8) detonates behind cannonball (5), thereby forms the motive force that cannonball (5) is quickened in cannonball (5) back.
8. ultra-high-speed gram-magnitude spherical projectile transmitting device according to claim 1, it is characterized in that, after described cannonball (5) was quickened for the first time by two-stage light gas gun (1), the high explosive of being ignited by annular steel disc (6) bump in three grades of accelerating cavities (10) (8) quickened once more.
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Cited By (10)
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| CN102221306A (en) * | 2011-06-15 | 2011-10-19 | 中国工程物理研究院流体物理研究所 | Ultrahigh-speed loading system of plane metal flying sheet |
| CN102778171A (en) * | 2012-07-24 | 2012-11-14 | 西北核技术研究所 | Three-level light-gas gun driven by compressed nitrogen |
| CN103673756A (en) * | 2013-11-13 | 2014-03-26 | 南京航空航天大学 | Vacuum chamber connecting device used for air cannon |
| CN104534924A (en) * | 2014-12-11 | 2015-04-22 | 哈尔滨工业大学 | Rotatable light-gas gun device |
| CN106644778A (en) * | 2016-10-21 | 2017-05-10 | 中国人民解放军空军第航空学院 | Multifunctional high-speed impact experimental equipment |
| CN106679500A (en) * | 2016-11-10 | 2017-05-17 | 北京理工大学 | Two-stage light gas gun driven through hydrogen energy |
| CN108286919A (en) * | 2018-01-23 | 2018-07-17 | 南京理工大学 | Detonation driven cumulative fragment generating means |
| CN108489334A (en) * | 2018-03-21 | 2018-09-04 | 中国工程物理研究院化工材料研究所 | A kind of High-velocity Projectiles emitter |
| CN115618772A (en) * | 2022-12-19 | 2023-01-17 | 中国空气动力研究与发展中心计算空气动力研究所 | Sharp front edge ultrahigh heat load dredging method based on high-temperature functional material catalytic regulation |
| CN115745711A (en) * | 2022-11-02 | 2023-03-07 | 北京卫星环境工程研究所 | Aluminum powder premixing reaction chamber for hydrogen-oxygen detonation driven light gas gun |
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| CN102221306A (en) * | 2011-06-15 | 2011-10-19 | 中国工程物理研究院流体物理研究所 | Ultrahigh-speed loading system of plane metal flying sheet |
| CN102778171A (en) * | 2012-07-24 | 2012-11-14 | 西北核技术研究所 | Three-level light-gas gun driven by compressed nitrogen |
| CN102778171B (en) * | 2012-07-24 | 2015-04-22 | 西北核技术研究所 | Three-level light-gas gun driven by compressed nitrogen |
| CN103673756A (en) * | 2013-11-13 | 2014-03-26 | 南京航空航天大学 | Vacuum chamber connecting device used for air cannon |
| CN103673756B (en) * | 2013-11-13 | 2015-10-28 | 南京航空航天大学 | Air bubble vacuum chamber jockey |
| CN104534924A (en) * | 2014-12-11 | 2015-04-22 | 哈尔滨工业大学 | Rotatable light-gas gun device |
| CN104534924B (en) * | 2014-12-11 | 2016-03-16 | 哈尔滨工业大学 | A kind of rotating light-gas gun device |
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| CN106644778A (en) * | 2016-10-21 | 2017-05-10 | 中国人民解放军空军第航空学院 | Multifunctional high-speed impact experimental equipment |
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| CN106679500B (en) * | 2016-11-10 | 2018-08-17 | 北京理工大学 | A kind of two-stage light gas gun driven with Hydrogen Energy |
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| CN108286919A (en) * | 2018-01-23 | 2018-07-17 | 南京理工大学 | Detonation driven cumulative fragment generating means |
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| CN115618772A (en) * | 2022-12-19 | 2023-01-17 | 中国空气动力研究与发展中心计算空气动力研究所 | Sharp front edge ultrahigh heat load dredging method based on high-temperature functional material catalytic regulation |
| CN115618772B (en) * | 2022-12-19 | 2023-03-07 | 中国空气动力研究与发展中心计算空气动力研究所 | Sharp leading edge ultrahigh heat load dredging method based on high-temperature functional material catalytic regulation |
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