CN101957159A - New high-thrust rocket - Google Patents
New high-thrust rocket Download PDFInfo
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- CN101957159A CN101957159A CN2009101604328A CN200910160432A CN101957159A CN 101957159 A CN101957159 A CN 101957159A CN 2009101604328 A CN2009101604328 A CN 2009101604328A CN 200910160432 A CN200910160432 A CN 200910160432A CN 101957159 A CN101957159 A CN 101957159A
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Abstract
The invention discloses a new high-thrust rocket, which comprises four types, namely, a space tower rocket (type 1), a liquefied metal fuel rocket (type 2), a pulse explosive rocket (type 3) and a massive-explosives pulse explosive rocket (type 4), wherein the space tower rocket (type 1) is characterized in that a set of jet nozzles (2) are arranged at intervals of certain height, and depending on ground pumping stations (7) and (8), various fuels are continuously conveyed by a pipe (5), combustion air does work to the jet nozzles to inject air to the ground direction to generate thrust so as to balance the layered loading of the space tower, thereby lead the space tower not to fall; the liquefied metal fuel rocket (type 2) is characterized in that an electric stove is used to liquefy flammable metals such as aluminum or aluminium alloy and the like at a high temperature; then the flammable metals subjected to liquefying are injected into a special insulating fuel tank (4) of the rocket and supplied for a rocket engine; the pulse explosive rocket (type 3) is characterized in that the thrust produced by the explosion of spherical explosives in a deflagration chamber (6) is used to promote the rocket to move on at a high speed; and the massive-explosives pulse explosive rocket (type 4) is characterized in that the thrusts produced by the explosion of massive explosives in a deflagration chamber (1) are used to promote the rocket to move on at a high speed. The type 2, 3 and 4 rockets can be used for building the space towers and space cities.
Description
[technical field] the present invention relates to novel thrust-augmented rocket, especially can be used as space city pillar and the space tower rocket that is connected platform.
[summary of the invention]
[type, space tower] the purpose of this invention is to provide a kind of safe in utilization, produces thrust with ducted rocket propulsion system or air nozzle, comes to bear a heavy burden for the layering of space tower the branch layer equilibration, the space tower that can succeed in developing on the theoretical foundation.
For achieving the above object, space tower of the present invention is by space tower body, by various gas transmissions, and air or oxygen or oxygen-enriched air and various liquid or gaseous fuel conveyance conduit.Various transmissions of electricity, communication, cable, express elevator or transport vehicle up and down, and various fuel and the gases at high pressure built on the circular orbit of ground carry pumping plant to form.The space tower is built on the ring-like motor-driven track, is to allow the space tower that certain maneuverability is arranged, can be by moving the bump that gets out of the way space trash and satellite and meteor shower.Need not move under the normal condition.The space tower is exactly the height of the best efficiency-cost ratio of vertical cylinder of a hollow in fact, in 2,000 kilometers, more than 200 kilometers, at a certain distance with one group of simple type ducted rocket propulsion system or air nozzle highly are installed, rely on ground pump station to carry various fuel continually by pipeline, combustion air or oxygen are given rocket engine or air nozzle acting, direction is jet earthward, produce thrust, come to bear a heavy burden, divide layer equilibration that it is not toppled over because of the weight of self for the layering of space tower.For fuel saving, the space tower can use electronic whirlpool oar or turbofan at lower, or the pressure-air nozzle ejects the cold high pressure air downwards and produce thrust, is that its layering is born a heavy burden and divided layer equilibration.Thereby reduce the diameter and the use cost of space tower.The space tower can be made assembling on ground, utilize the whole lifting of the dynamical system of himself can verting then.
(effect and purposes)
Can be used for communication, scout, solar electrical energy generation, new material is processed, space flight, aerospace, astronomy, space metallurgy, the exploitation space resources is built space city, and can be used for military affairs and launch a guided missile, satellite, the space station, emission laser, extensive space is lived and is traveled.The space tower reach a certain height, because away from terrestrial gravitation, because earth rotation gravitation diminishes weight saving or disappearance.
[two types, liquefaction metal fuel type rocket] is characterized in that using electric furnace, and with the high temperature combustible metal that liquefies, as aluminum or aluminum alloy etc., the special-purpose thermal insulation fuel tank that rocket is injected in the liquefaction back uses for rocket engine.The purpose of liquefaction is to allow petrolift can extract fuel.After taking off, uses by rocket the fuel insulation, jet pipe cooling hot recycle pump.Fuel can not solidified, also lower the temperature simultaneously to jet pipe.
The benefit of using high temperature liquefaction combustible metal to do rocket fuel is that it is safe and efficient at a low price, and high initial temperature is burnt easily, high density.Its density is far above liquid hydrogen, and without pressure steel cylinder, so under the identical situation of volume tonnage, little more than the rocket volume that uses other liquid fuel, the load height.The speed of this kind rocket is very fast, generally just can reach the first universal speed in the endoatmosphere, more than per second eight kms.So this kind rocket adopts special head design, it is characterized in that adopting double-deck hollow radome fairing, allow air enter to reduce and discharge after flowing velocity prolongs the cooling of its heat absorption time, thereby play the effect of cooling off head from rocket nose section.
The recoil that [three types, pellet powder pulse explosion type rocket] is characterized in that using pellet powder to explode in the detonation chamber and produce promotes that rocket advances at utmost speed.Operation principle is, pellet powder falls naturally from the funnel-form fuel tank bottom, or draws in the convertible ready service magazine of getting the bullet machine with the series connection rope, gets the bullet machine after shooting and turns over after the turnback in the detonation chamber that ignition charge produces reaction force and thrust advances at utmost speed rocket.Per minute work acting number of times is controlled automatically by computer.The medium-and-large-sized rocket of practice has a plurality of detonations chamber.
Because rocket of the present invention uses the high-purity explosive, littler, in light weight than the solid-rocket volume of other kind, the working time is long, the load height.And the parking ability of aloft arbitrarily driving is arranged, and for preventing the too high rocket of wound of impulsive force,, when resetting, buffer also can produce certain thrust so efficient buffer is housed, and the head type of cooling is with two types.
The recoil that [four types, block explosive pulse explosion type rocket] is characterized in that using block explosive to explode in the explosion type combustion chamber and produce, just reaction force promotes that rocket advances at utmost speed.Block explosive is fixed in the fuel tank by magnetic or tongue and groove or extraordinary glue or bolt-type detonator.
To be automatic filling machine with the explosive piece take off to send in the detonation chamber and automatically from fuel tank operation principle ignites, and produces reaction force and thrust rocket is advanced at utmost speed.In order to increase reliability, automatic filling machine has multi-section in the practice.Other is with three types, and the rocket nose section type of cooling is with two types.
Above-mentioned two, three, four type rockets can be used for transporting material, build space tower and space city, also can be used for launching an artificial satellite or guided missile.
[description of drawings] the present invention is further detailed explanation below in conjunction with the drawings and specific embodiments,
" accompanying drawing is the cutaway view and the schematic diagram of the novel thrust-augmented rocket of the present invention.”
[type] workbench 1.Simple type ducted rocket propulsion system or air nozzle 2.Space tower body 3.Transmission cable and communication cable 4.Various fuel and gases at high pressure conveyance conduit 5.Express elevator or transport vehicle 6 up and down.7 and 8 fuel and gases at high pressure are carried pumping plant.Intermediate booster pump 9.The space column foot sits 10.The motor-driven track 11 of annular.
[two types] air enters 1 from the head.Cooling back air discharges 2.Load 3.The liquefaction metal, fuel incubator 4.The fuel insulation, jet pipe cooling hot recycle pump 5.Petrolift 6.Rocket engine and jet pipe 7.
[three types] pellet powder 4.The generator 5 of buffer and its drive.Detonation chamber and jet pipe 6.Automatic control mechanism 7.Tandem pellet powder and ready service magazine 8.1 and 2 with two types.The automatic convertible bullet machine 9 of getting by buffer bent axle or Electric Machine Control.
[four types] buffer 4.Intelligent automatic getting plays pawl 5.Get and play loader 6.Block explosive 7.The generator 8 of buffer and its drive.Get the power motor and the automatic control mechanism 9 of bullet dress prototype.Detonation chamber and jet pipe 10.1 and 2 with two types.
[five types] global space city schematic diagram.
Global space city 1.Space tower 2.The earth 3.
Claims (8)
1. novel thrust-augmented rocket,
[type, the space tower] it is characterized in that: described space tower body (3), by various gas transmissions, pressure-air or oxygen or oxygen-enriched air, with various liquid, or gaseous fuel conveyance conduit (5), various transmission of electricity, communication, cable (4), express elevator or transport vehicle (6) and build various fuel on the circular orbit of ground in and gases at high pressure are carried pumping plants (7) and (8) composition are built the space tower on the circular orbit (11) up and down, are to allow the space tower that certain maneuverability is arranged.
2. novel thrust-augmented rocket according to claim 1, the space tower
It is characterized in that: described space tower at a certain distance with one group of simple type ducted rocket propulsion system highly is installed, or air nozzle (2), rely on ground pump station to carry various fuel continually by pipeline, combustion air or oxygen are given the acting of rocket engine or air nozzle, and direction is jet earthward, produce thrust, come to bear a heavy burden, divide layer equilibration, it is not toppled over because of the weight of self for the layering of space tower.
3. a novel thrust-augmented rocket [two types, liquefaction metal fuel type rocket],
It is characterized in that: use electric furnace, with the high temperature combustible metal that liquefies, as aluminum or aluminum alloy etc., the special-purpose thermal insulation fuel tank (4) that rocket is injected in the liquefaction back uses for rocket engine, and the purpose of liquefaction is to allow petrolift can extract fuel, after taking off, uses by rocket the fuel insulation, the jet pipe cooling can not solidify fuel with hot recycle pump (5), also gives jet pipe (7) cooling simultaneously.
4. according to the described rocket of claim 3,
It is characterized in that: be to adopt double-deck hollow radome fairing, allow air enter (1) from the head, prolong its heat absorption time, (2) are discharged in the cooling back, thereby play the effect of cooling head.
5. a novel thrust-augmented rocket [three types, pellet powder pulse explosion type rocket],
It is characterized in that: the recoil that uses pellet powder (4) to explode in detonation chamber and jet pipe (6) and produce promotes rocket and advances at utmost speed.
6. according to the described rocket of claim 5,
It is characterized in that: pellet powder falls naturally from the funnel-form fuel tank bottom, or draw in the convertible ready service magazine (9) of getting the bullet machine with series connection rope, get the bullet machine after shooting and turn over after the turnback ignition charge in the detonation chamber, for preventing the too high rocket of wound of impulsive force, so efficient buffer (5) is housed, the head type of cooling (1) and (2) are with two types.
7. the block explosive pulse explosion type of a novel thrust-augmented rocket [four types] rocket,
It is characterized in that: the recoil that is to use block explosive (7) to explode in detonation chamber and jet pipe (10) to produce promotes that rocket advances at utmost speed.
8. according to the described rocket of claim 7,
It is characterized in that: intelligent automatic getting plays pawl (5), gets and plays loader (6), and buffer (8) is got power motor and automatic control mechanism (9) the head type of cooling (1) and (2) same [two types] of playing loader.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101604328A CN101957159A (en) | 2009-07-13 | 2009-07-13 | New high-thrust rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101604328A CN101957159A (en) | 2009-07-13 | 2009-07-13 | New high-thrust rocket |
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| Publication Number | Publication Date |
|---|---|
| CN101957159A true CN101957159A (en) | 2011-01-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009101604328A Pending CN101957159A (en) | 2009-07-13 | 2009-07-13 | New high-thrust rocket |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104929809A (en) * | 2015-06-04 | 2015-09-23 | 杜善骥 | Working method of detonation ram rocket |
| CN109900478A (en) * | 2019-03-18 | 2019-06-18 | 西安爱生技术集团公司 | A kind of small and medium size unmanned aerial vehicles rocket thrust test device and test method |
| CN110284995A (en) * | 2019-06-14 | 2019-09-27 | 北京理工大学 | A kind of disk transfer type locellus solid propellant rocket |
| CN113803190A (en) * | 2021-09-26 | 2021-12-17 | 宁波天擎航天科技有限公司 | Solid fuel ramjet engine |
| CN114194419A (en) * | 2021-11-29 | 2022-03-18 | 北京空间机电研究所 | Parachute system suitable for carrier rocket radome recovery |
-
2009
- 2009-07-13 CN CN2009101604328A patent/CN101957159A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104929809A (en) * | 2015-06-04 | 2015-09-23 | 杜善骥 | Working method of detonation ram rocket |
| CN109900478A (en) * | 2019-03-18 | 2019-06-18 | 西安爱生技术集团公司 | A kind of small and medium size unmanned aerial vehicles rocket thrust test device and test method |
| CN109900478B (en) * | 2019-03-18 | 2020-09-25 | 西安爱生技术集团公司 | Device and method for testing rocket thrust of small and medium-sized unmanned aerial vehicles |
| CN110284995A (en) * | 2019-06-14 | 2019-09-27 | 北京理工大学 | A kind of disk transfer type locellus solid propellant rocket |
| CN113803190A (en) * | 2021-09-26 | 2021-12-17 | 宁波天擎航天科技有限公司 | Solid fuel ramjet engine |
| CN113803190B (en) * | 2021-09-26 | 2022-08-26 | 宁波天擎航天科技有限公司 | Solid fuel ramjet engine |
| CN114194419A (en) * | 2021-11-29 | 2022-03-18 | 北京空间机电研究所 | Parachute system suitable for carrier rocket radome recovery |
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Application publication date: 20110126 |