CN106428654A - Small-sized split type survivable deep space impactor - Google Patents
Small-sized split type survivable deep space impactor Download PDFInfo
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- CN106428654A CN106428654A CN201611021569.1A CN201611021569A CN106428654A CN 106428654 A CN106428654 A CN 106428654A CN 201611021569 A CN201611021569 A CN 201611021569A CN 106428654 A CN106428654 A CN 106428654A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G4/00—Tools specially adapted for use in space
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- Geophysics And Detection Of Objects (AREA)
Abstract
The invention discloses a small-sized split type survivable deep space impactor which comprises a front part and a rear part. The front part and the rear part are connected through a connection cable and are jointed into a whole before impacting and separated after impacting. The front part comprises a front part body, a head cap, an air bottle, a navigation sensor and a propeller, the navigation sensor is mounted in the head cap which is mounted at the top end of the front part body, the air bottle is mounted in the front part body, and the propeller is mounted on the inner side wall of the front part body. The rear part comprises a rear part body, an air bag, an electronic module and a buffer module, the buffer module is mounted in the rear part body to form a structural support of the rear part body, the air bag is mounted on the periphery of the buffer module, and the electronic module is mounted at the top of the rear part body to form an integral module by filling and sealing. The small-sized split type survivable deep space impactor is capable of penetrating into a target and survived, and accurate impacting can be realized through controllable flight. In addition, the deep space impactor is integrally compact in design, high in stability and adaptive to demands of survivable deep space impact detection in the future.
Description
Technical field
The present invention relates to earth satellite or other deep space exploration aircraft fields, specifically a kind of small-sized split type survive
Deep space ram.
Background technology
Development with space technology and progress, the means of survey of deep space are developed into cincture, by the initial detection that leaps
The multimode combined detection such as land, tour, sampling, realize be around to landings, surface to inside leap, to three-dimensional probe,
Internal depth detection direction develops.
Impact probing is the efficient means realizing internal detection, has that simple and reliable for structure, integrated level is high, flexible configuration
Feature, consumes fewer resource and gets final product penetration to inside celestial body.
Clash into Penetration detector to be impacted by high overload, internal electronic equipment faces the risk of damage, using small-sized
Split-type design, can improve Penetration Depth, reduce the shock loading of electronic equipment, after being advantageously implemented deep space high-speed impact
Existence.
Content of the invention
The present invention is directed to the feature of deep space high-speed impact detection mission, there is provided a kind of small-sized split type deep space of surviving hits
Hit device it is ensured that detector can clash into target with certain precision, penetration to inside and survives development detected event.
The purpose of the present invention is achieved through the following technical solutions：A kind of small-sized split type deep space ram of surviving, bag
Included the precursor of connection cables connection and rear body, described precursor is coupled as one before shock with rear body, separates after shock；Described
Precursor includes precursor body, head-shield, gas cylinder, navigation sensor and propeller, and described head-shield is arranged on the top of precursor body, interior
Portion is provided with described navigation sensor, and described gas cylinder is arranged on the inside of precursor body, and described propeller is arranged on precursor body
Madial wall on；Described rear body includes rear body body, air bag, electronic module, buffer module, and described buffer module is arranged on rear body
This is internal, the structural support of body body after composition, and described air bag is arranged on the periphery of buffer module, and described electronic module is arranged on
Body bodies top afterwards, forms integral module by embedding.
Preferably, described precursor is originally also equipped with sensor in vivo, and sensor is connected with electronic module by connection cables,
Carry out information exchange.
Preferably, it is provided with parting surface at described precursor body upper end open.
Preferably, described buffer module is combined by two kinds of padded coamings and is formed by stacking.
Preferably, described electronic module adopts overall package form.
Compared with prior art, the invention has the advantages that：
Penetration can be met to target internal and survive, pass through controllable flight simultaneously and can achieve accurately shock, whole deep space
Ram is compact to design, good stability, adapts to following deep space and can survive the demand of impact probing.
Brief description
Fig. 1 is a kind of exploded perspective schematic diagram of small-sized split type deep space ram of surviving of the embodiment of the present invention.
Fig. 2 is a kind of Structure explosion diagram of small-sized split type deep space ram of surviving of the embodiment of the present invention.
Fig. 3 is a kind of state of flight structural representation of small-sized split type deep space ram of surviving of the embodiment of the present invention.
Fig. 4 is a kind of emission state structural representation of small-sized split type deep space ram of surviving of the embodiment of the present invention.
Fig. 5 is a kind of emission state profile of small-sized split type deep space ram of surviving of the embodiment of the present invention.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, some deformation can also be made and improve.These broadly fall into the present invention
Protection domain.
As Figure 1-Figure 5, embodiments provide a kind of small-sized split type deep space ram of surviving, including
Precursor 1 and rear body 2 that connection cables 3 connect, described precursor is coupled as one before shock with rear body, separates after shock；Described
Precursor 1 includes precursor body 13, head-shield 11, gas cylinder 14, navigation sensor 12 and propeller 15, and described head-shield 11 is arranged on precursor
The top of body 13, inside is provided with described navigation sensor 12, and described gas cylinder 14 is arranged on the inside of precursor body 13, described
Propeller 15 is arranged on the madial wall of precursor body 13；Described rear body 2 include rear body body 23, air bag 24, electronic module 21,
Buffer module 25, described buffer module 25 is arranged in rear body body 23, the structural support of body body 23 after composition, described air bag
24 peripheries being arranged on buffer module 25, enter state of flight rear gasbag inflating expanded one-tenth ball crown type, and described electronic module 21 is pacified
It is contained in rear body body 23 top, integral module is formed by embedding.
It is also equipped with sensor 16, sensor 16 passes through connection cables 3 and electronic module 21 phase in described precursor body 13
Even, carry out information exchange.
It is provided with parting surface 4 at described precursor body 13 upper end open.
Described buffer module is combined by two kinds of padded coamings and is formed by stacking.
Described electronic module 21 adopts overall package form.
Wherein, under described air bag state of flight inflating expanded in ball crown type, envelope size：Long 70cm, precursor 3 diameter of phi
10cm, rear body 1 diameter of phi 20cm, largest diameter 60cm；Emission state lower gasbag draws in around rear body body, envelope chi
Very little：Long 70cm, maximum gauge 25cm.
Originally it is embodied as meeting the requirement clashed into penetration and survive simultaneously, using split-type design, clash in ram
Precursor is separated with rear body afterwards, and rear body reduces, by buffer module, the overload impact that electronic module is subject to, using the gas of deployed condition
After capsule stops, body enters inside impact crater, provides the area needed for laying solar cell piece simultaneously；Precursor relies on inertia penetration to arrive
Inside soil, internal detection is carried out by sensor, obtain data.
Above the specific embodiment of the present invention is described.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various modifications or modification within the scope of the claims, this not shadow
Ring the flesh and blood of the present invention.
Claims (5)
1. a kind of small-sized split type survive deep space ram it is characterised in that：Including connection cables connect precursor and after
Body, described precursor is coupled as one before shock with rear body, separates after shock；Described precursor includes precursor body, head-shield, gas
Bottle, navigation sensor and propeller, described head-shield is arranged on the top of precursor body, and inside is provided with described navigation sensor,
Described gas cylinder is arranged on the inside of precursor body, and described propeller is arranged on the madial wall of precursor body；Described rear body includes
Body body, air bag, electronic module, buffer module afterwards, described buffer module is arranged on rear body originally in vivo, knot of body body after composition
Structure supports, and described air bag is arranged on the periphery of buffer module, and described electronic module is arranged on rear body bodies top, by embedding shape
Integral module.
2. one kind as claimed in claim 1 small-sized split type survive deep space ram it is characterised in that：Described precursor body
Inside it is also equipped with sensor, sensor is connected with electronic module by connection cables, carry out information exchange.
3. one kind as claimed in claim 1 small-sized split type survive deep space ram it is characterised in that：Described precursor body
It is provided with parting surface at upper end open.
4. one kind as claimed in claim 1 small-sized split type survive deep space ram it is characterised in that：Described buffer module
Combined by two kinds of padded coamings and be formed by stacking.
5. one kind as claimed in claim 1 small-sized split type survive deep space ram it is characterised in that：Described electronic module
Using overall package form.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611021569.1A CN106428654B (en) | 2016-11-17 | 2016-11-17 | A kind of small-sized split type deep space ram of surviving |
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| CN201611021569.1A CN106428654B (en) | 2016-11-17 | 2016-11-17 | A kind of small-sized split type deep space ram of surviving |
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| CN106428654A true CN106428654A (en) | 2017-02-22 |
| CN106428654B CN106428654B (en) | 2019-01-08 |
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Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN108820261A (en) * | 2018-06-20 | 2018-11-16 | 上海卫星工程研究所 | A kind of separation tripper for slender type ram |
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN109398766A (en) * | 2018-11-29 | 2019-03-01 | 哈尔滨工业大学 | A kind of trajectory buffer-type star landing and scientific exploration platform |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
| CN111409872A (en) * | 2020-03-06 | 2020-07-14 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space impactor |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| CN111547276A (en) * | 2020-03-31 | 2020-08-18 | 上海卫星工程研究所 | Intelligent autonomous temperature control structure and temperature control method for deep space impactor |
| CN111591464A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Deep space impactor and impact protection performance evaluation method thereof |
| CN111654332A (en) * | 2020-03-31 | 2020-09-11 | 上海卫星工程研究所 | Deep-buried equivalent communication test system after deep space impactor hits |
| CN111661367A (en) * | 2020-07-31 | 2020-09-15 | 北京控制与电子技术研究所 | Autonomous navigation flight control system for deep space impact |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN111731516A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Miniaturized survivable intelligent deep space high-speed impactor |
| CN114084376A (en) * | 2021-11-18 | 2022-02-25 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star catalogue emission |
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| CN103419945A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with escapement mechanism |
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| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
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| JPH03118300A (en) * | 1989-10-02 | 1991-05-20 | Natl Space Dev Agency Japan<Nasda> | Alignment device for structure |
| CN102501986A (en) * | 2011-09-27 | 2012-06-20 | 南京航空航天大学 | Anchoring and sampling mechanism of planetary probe |
| CN103419945A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with escapement mechanism |
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Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN108820261A (en) * | 2018-06-20 | 2018-11-16 | 上海卫星工程研究所 | A kind of separation tripper for slender type ram |
| CN108820261B (en) * | 2018-06-20 | 2020-07-14 | 上海卫星工程研究所 | Separation unlocking device for slender type impactor |
| CN109398766A (en) * | 2018-11-29 | 2019-03-01 | 哈尔滨工业大学 | A kind of trajectory buffer-type star landing and scientific exploration platform |
| CN109398766B (en) * | 2018-11-29 | 2021-07-20 | 哈尔滨工业大学 | Ballistic buffering type planet landing and scientific detection platform |
| CN109677633B (en) * | 2019-01-17 | 2020-07-28 | 上海卫星工程研究所 | Small-sized high-speed impactor for physically destroying surface structure of extraterrestrial celestial body |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
| CN111409872B (en) * | 2020-03-06 | 2020-11-24 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space impactor |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| CN111409872A (en) * | 2020-03-06 | 2020-07-14 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space impactor |
| CN111591464A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Deep space impactor and impact protection performance evaluation method thereof |
| CN111654332A (en) * | 2020-03-31 | 2020-09-11 | 上海卫星工程研究所 | Deep-buried equivalent communication test system after deep space impactor hits |
| CN111547276A (en) * | 2020-03-31 | 2020-08-18 | 上海卫星工程研究所 | Intelligent autonomous temperature control structure and temperature control method for deep space impactor |
| CN111654332B (en) * | 2020-03-31 | 2022-05-10 | 上海卫星工程研究所 | Deep-buried equivalent communication test system after deep space impactor hits |
| CN111547276B (en) * | 2020-03-31 | 2021-12-03 | 上海卫星工程研究所 | Intelligent autonomous temperature control structure and temperature control method for deep space impactor |
| CN111661367A (en) * | 2020-07-31 | 2020-09-15 | 北京控制与电子技术研究所 | Autonomous navigation flight control system for deep space impact |
| CN111731516B (en) * | 2020-07-31 | 2020-11-17 | 北京控制与电子技术研究所 | Miniaturized survivable intelligent deep space high-speed impactor |
| CN111731511B (en) * | 2020-07-31 | 2020-11-17 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN111731516A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Miniaturized survivable intelligent deep space high-speed impactor |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN114084376A (en) * | 2021-11-18 | 2022-02-25 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star catalogue emission |
| CN114084376B (en) * | 2021-11-18 | 2023-12-22 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star meter emission |
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