JP5927459B1 - Launch pad for small rocket - Google Patents

Launch pad for small rocket Download PDF

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JP5927459B1
JP5927459B1 JP2015117843A JP2015117843A JP5927459B1 JP 5927459 B1 JP5927459 B1 JP 5927459B1 JP 2015117843 A JP2015117843 A JP 2015117843A JP 2015117843 A JP2015117843 A JP 2015117843A JP 5927459 B1 JP5927459 B1 JP 5927459B1
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rocket
small
launch pad
thrust
rockets
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JP2016217687A (en
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敦 石原
敦 石原
真也 中原
真也 中原
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Abstract

【課題】小型ロケット用発射台を提供する。【解決手段】小型ロケット用発射台の主な構造は、下部支持板、脚、ロケットガイド、上部板、推力測定部、保護板からなる。小型ロケットを本発射台に設置し、本発射台でロケット発射実験を行うことにより、室内でも安全にロケットの飛しょうをデモンストレーションしながら同時に飛しょう中のロケット推力も測定できる。【選択図】図1A launch pad for a small rocket is provided. The main structure of a launch pad for a small rocket is composed of a lower support plate, legs, a rocket guide, an upper plate, a thrust measuring unit, and a protective plate. By installing a small rocket on the launch pad and conducting a rocket launch experiment on the launch pad, it is possible to measure the rocket thrust during the flight while demonstrating the rocket flying safely indoors. [Selection] Figure 1

Description

本発明は、小型ロケット用発射台に関する。    The present invention relates to a launch pad for a small rocket.

従来は,ペットボトルロケットやモデルロケットや玩具ロケット等の小型ロケット用発射台は、屋外に設置されているため、ロケットの飛しょう実験は天候に左右され、強風時や豪雨時には実験の実施が困難であった。  Conventionally, small rocket launchpads such as plastic bottle rockets, model rockets, and toy rockets are installed outdoors, so rocket flight experiments are influenced by the weather, and it is difficult to conduct experiments during strong winds or heavy rains. Met.

また、ペットボトルロケットやモデルロケットや玩具ロケット等の小型ロケット性能は,到達高度あるいは飛しょう距離より算出し、飛しょうしながらの推力の計測は行われていなかった。  The performance of small rockets such as plastic bottle rockets, model rockets, and toy rockets was calculated from the altitude reached or the flight distance, and the thrust was not measured while flying.

特開平11−327474号公報Japanese Patent Laid-Open No. 11-327474 特開平9−294874号公報JP-A-9-294874

上記の問題点を解決するため、天候に関係ない屋内でも、太さの異なるペットボトルロケットやモデルロケットや玩具ロケット等の小型ロケットの飛しょうデモンストレーションとロケット推力測定が、安全にできるようにする必要がある。  In order to solve the above problems, it is necessary to be able to safely perform flying demonstration and measurement of rocket thrust of small rockets such as plastic bottle rockets, model rockets and toy rockets of different thickness even indoors regardless of the weather There is.

本発明は上記目的である室内においても安全に小型ロケットのデモンストレーション行うことを達成するために、本発明の小型ロケット用発射台は、発射前の小型ロケットを支える下部支持板、発射台を支える脚、ロケットの発射後の飛しょう経路を制限するロケットガイド、ロケット飛しょう時の推力を受ける上部板から構成されている。  In order to achieve the demonstration of a small rocket safely in the room, which is the object of the present invention, the launch pad for the small rocket of the present invention includes a lower support plate that supports the small rocket before launch, and a leg that supports the launch pad. It consists of a rocket guide that restricts the flight path after launching the rocket, and an upper plate that receives thrust during the launch of the rocket.

太さの異なる小型ロケットでも安全に飛しようさせるため、上部板と下部支持板には、ロケットガイド間隔を調整できる調整用スリットを、板中心から放射状に設けることができる。  In order to allow even small rockets of different thicknesses to fly safely, the upper plate and the lower support plate can be provided with adjustment slits that can adjust the rocket guide interval radially from the plate center.

予期しないロケットの破裂による飛散物から観測者を守るための保護板を設置することができる。  A protective plate can be installed to protect the observer from flying objects caused by unexpected rocket explosions.

飛しょう中のロケットの推力を測定するために、上部板略中央に推力測定のための推力測定器を設けることができる。  In order to measure the thrust of the flying rocket, a thrust measuring device for measuring the thrust can be provided in the approximate center of the upper plate.

以上、説明したように、本発明によれば、室内外でのロケットの飛しょう実験の実施も可能であるが、天候に関係なく室内で安全にロケット飛しょう実験のデモンストレーションを行うことができるため、室内で行われるロケット教育体験教材としても利用することができる。  As described above, according to the present invention, it is possible to carry out a rocket flight experiment indoors and outdoors, but it is possible to demonstrate a rocket flight experiment safely indoors regardless of the weather. It can also be used as a teaching material for rocket education in the room.

また、太さの異なる小型ロケットの飛しょう実験の場合にも容易に安全に対応できる効果がある。 In addition , there is an effect that can be easily and safely dealt with in a flight experiment of small rockets of different thicknesses.

請求項によれば、予期しない小型ロケットの破裂による飛散物から観測者を守ることができるため、特に安全が重要な室内で行われるロケット教育体験教材としても利用することができる。According to the second aspect , since the observer can be protected from the flying object due to the unexpected explosion of the small rocket, it can be used as a teaching material for a rocket education experience that is performed in a room where safety is particularly important.

請求項によれば、上部板略中央に推力測定器を設置することにより、小型ロケット飛しょう中の推力測定ができる。According to the third aspect of the present invention, the thrust measurement device can be measured while flying a small rocket by installing a thrust measuring device substantially at the center of the upper plate.

本発明の小型ロケット用発射台の斜視図  The perspective view of the launch pad for the small rocket of the present invention 図1から小型ロケットを除いた発射台の斜視図  1 is a perspective view of the launch pad without a small rocket from FIG. 図1の小型ロケットが飛しょうしている状態の発射台の概略図  Schematic of the launch pad with the small rocket in Fig. 1 flying 図1の発射台の下部支持板の平面図  Plan view of the lower support plate of the launch pad of FIG. 図1の発射台に保護板を設置した斜視図  1 is a perspective view of a protective plate installed on the launch pad of FIG. 推力測定器を設置した小型ロケット用発射台の正面図  Front view of a launch pad for a small rocket equipped with a thrust meter 本発明の発射台を横向きに設置した場合の発射台の正面図  Front view of launch pad when launch pad of the present invention is installed sideways

図1は、本発明の小型のロケット用発射台の基本形態である。図1の小型ロケット1は、ペットボトルロケットやモデルロケットや玩具ロケット等の推力が20kgf以下の小推力ロケットである。  FIG. 1 shows a basic form of a launch pad for a small rocket according to the present invention. The small rocket 1 in FIG. 1 is a small thrust rocket having a thrust of 20 kgf or less, such as a plastic bottle rocket, a model rocket, a toy rocket, or the like.

図1の2は下部支持板であり,図2のように下部支持板2の中心には、ロケットの太さより小さい直径を持つロケット設置穴3が開けられており、図1のように発射前の小型ロケット1を安定して置くことができる。  Reference numeral 2 in FIG. 1 denotes a lower support plate. A rocket installation hole 3 having a diameter smaller than the thickness of the rocket is formed in the center of the lower support plate 2 as shown in FIG. The small rocket 1 can be placed stably.

下部支持板2の下には脚4がある。適当な長さの脚4を選択することにより、発射前のロケットの位置を程良い高さに設置できる。  Below the lower support plate 2 is a leg 4. By selecting the leg 4 having an appropriate length, the position of the rocket before launching can be installed at a moderate height.

下部支持板2には、ロケットガイド5が設置されており、ロケットガイド5のそれぞれがほぼ平行になるように、上部板6でロケットガイド5を固定している。  A rocket guide 5 is installed on the lower support plate 2, and the rocket guide 5 is fixed by an upper plate 6 so that the rocket guides 5 are substantially parallel to each other.

ロケットガイド5の両端には、例えば、ねじが切ってあり、下部支持板2および上部板6とロケットガイド5とをナット等で固定する。このことで発射台の分解やロケットガイド5を容易に交換することもできる。  For example, screws are cut at both ends of the rocket guide 5, and the lower support plate 2 and the upper plate 6 and the rocket guide 5 are fixed with nuts or the like. Thus, the launch pad can be disassembled and the rocket guide 5 can be easily replaced.

小型ロケット1は、発射後、ロケットガイド5に沿って上昇し、上部板6に当たる。その状態を、図3の概略図に示す。  After launch, the small rocket 1 rises along the rocket guide 5 and hits the upper plate 6. This state is shown in the schematic diagram of FIG.

下部支持板2の平面図を図4に示す。図4の8の円は、図1の小型ロケット1の断面の外形円で小型ロケットの最大の太さを示すものである。図4におけるロケットガイドの間隔aおよびbは、ロケットの太さを示す円8の直径cよりわずかに狭くなっており,ロケットガイド5の間からロケットが飛び出さないようになっている。そのため室内でもロケットの飛しょう実験が可能となる。  A plan view of the lower support plate 2 is shown in FIG. The circle 8 in FIG. 4 is the outer circle of the cross section of the small rocket 1 in FIG. 1 and indicates the maximum thickness of the small rocket. The intervals a and b of the rocket guides in FIG. 4 are slightly narrower than the diameter c of the circle 8 indicating the thickness of the rocket, so that the rockets do not jump out between the rocket guides 5. This makes it possible to conduct rocket flight experiments even indoors.

図1には4本のロケットガイド5が描かれているが、ロケットガイドの数は多いほうが安全性の上では好ましい。ただし,最低3本のロケットガイドがあれば、本発明によるロケット飛しょう実験は安全に実施可能である。  Although four rocket guides 5 are depicted in FIG. 1, it is preferable in terms of safety that the number of rocket guides is large. However, if there are at least three rocket guides, the rocket flight experiment according to the present invention can be carried out safely.

図4の下部支持板2には、ロケットガイド間の間隔を調節するための調整用スリット(下部)9が,ロケットガイド5の数に合わせ板の中心から放射状に設けられている。同様なスリットが図5の上部板6にも設けられている。  In the lower support plate 2 of FIG. 4, adjustment slits (lower portions) 9 for adjusting the distance between the rocket guides are provided radially from the center of the plate according to the number of rocket guides 5. Similar slits are provided in the upper plate 6 of FIG.

したがって、図5の下部支持板2に設けられた調整用スリット(下部)9と、図5の上部板5に設けられた調整用スリット(上部)10によるロケットガイド間隔の調節により、異なった太さを持つロケットでも、その飛しょうを、ロケットガイド5内に制限することができる。  Accordingly, adjustment of the rocket guide interval by the adjustment slit (lower part) 9 provided in the lower support plate 2 in FIG. 5 and the adjustment slit (upper part) 10 provided in the upper plate 5 in FIG. Even a rocket having a height can be restricted within the rocket guide 5.

図5のように、発射台に透明なポリカーボネート等の強固な透明プラスチック製の保護板11を、保護板取り付け治具13等を用いて発射台とほぼ平行になるように設置すれば、ロケットが予期しない破裂をしても、ロケットの破片が観察者のほうへ飛散しないようにできるため、室内で行われるロケット教育体験教材としても利用することができる。  As shown in FIG. 5, if a protective plate 11 made of transparent transparent plastic such as polycarbonate is placed on the launch pad so as to be substantially parallel to the launch pad using the protective plate mounting jig 13 or the like, Even if an unexpected rupture occurs, the rocket fragments can be prevented from scattering toward the observer.

図6は、本発明の小型ロケット用発射台の上部板5の下側に推力測定器12を設置した正面図である。図6の推力測定器12は、測定器にかかる力を電気信号に変換するものであり,測定器に市販のロードセルを使用するか、または,上部板にかかる推力によるひずみを、ひずみゲージとひずみ測定器を使用することで、測定器にかかる力を測定することができる。  FIG. 6 is a front view in which a thrust measuring device 12 is installed on the lower side of the upper plate 5 of the launch pad for a small rocket of the present invention. The thrust measuring instrument 12 shown in FIG. 6 converts the force applied to the measuring instrument into an electric signal. A commercially available load cell is used for the measuring instrument, or the strain due to the thrust applied to the upper plate is determined by a strain gauge and a strain. By using the measuring device, the force applied to the measuring device can be measured.

したがって、上部板略中央に推力測定器を設置することにより、ロケット飛しょう中の推力測定ができる。  Therefore, it is possible to measure the thrust during the rocket flight by installing a thrust measuring device in the approximate center of the upper plate.

ロケット発射時の推力測定の誤差を小さくしたい場合には、図6のロケットガイド5の長さを短くする。ロケット飛しょうデモンストレーションの際の迫力を優先させたい場合には、ロケットガイド5を長くすると迫力がより増し、使用目的に応じて、ロケットガイド5の長さを変えたりし、上部板6と下部支持板2の間隔を調節する。  When it is desired to reduce the error in thrust measurement at the time of launching the rocket, the length of the rocket guide 5 in FIG. 6 is shortened. If you want to prioritize the force of the rocket flight demonstration, the longer the rocket guide 5, the more powerful it will be. Depending on the purpose of use, the length of the rocket guide 5 may be changed, and the upper plate 6 and lower support The distance between the plates 2 is adjusted.

また、室外で、ロケットの飛しょうを行う場合には、上部板6を外すことにより、従来のロケット発射台のようにロケットを空中に射出することもできる。  In addition, when flying a rocket outdoors, the rocket can be injected into the air like a conventional rocket launch pad by removing the upper plate 6.

さらに、上部板6と下部支持板2の形状を、各板1辺の長さが等しい長方形等にすれば、図7のように水平燃焼実験も容易に実施できる。  Furthermore, if the shapes of the upper plate 6 and the lower support plate 2 are made into rectangles having the same length of one side of each plate, a horizontal combustion experiment can be easily performed as shown in FIG.

1 小型ロケット
2 下部支持板
3 ロケット設置穴
4 脚
5 ロケットガイド
6 上部板
7 飛しょう中の小型ロケット
8 ロケットの太さを示す円
9 調節用スリット(下部)
10 調節用スリット(上部)
11 保護板
12 推力測定器
13 保護板取り付け治具
DESCRIPTION OF SYMBOLS 1 Small rocket 2 Lower support plate 3 Rocket installation hole 4 Leg 5 Rocket guide 6 Upper plate 7 Small rocket in flight 8 Circle indicating thickness of rocket 9 Adjustment slit (lower part)
10 Adjustment slit (top)
11 Protection plate 12 Thrust measuring instrument 13 Protection plate mounting jig

Claims (3)

推力が20kgf以下の小型ロケット用発射台であって、発射前の小型ロケットを支える下部支持板と脚、発射後の小型ロケットの飛しょう経路を制限するロケットガイド、小型ロケットの推力を受ける上部板からなり、小型ロケットの太さによって、ロケットガイド間の間隔を調整し、太さの異なる小型ロケットでも安全に小型ロケットを飛しょうさせるための調整スリットが上部板と下部支持板にそれぞれ板の中心から放射状に設けられていることを特徴とする小型ロケット用発射台。A launch pad for a small rocket with a thrust of 20 kgf or less, a lower support plate and legs that support the small rocket before launch, a rocket guide that restricts the flight path of the small rocket after launch, and an upper plate that receives the thrust of the small rocket Tona is, depending on the thickness of the small rockets, to adjust the spacing between rockets guide, adjusting a slit for causing the flying safely small rockets in different small rockets of thickness of each plate to the upper plate and the lower support plate small rocket launcher you and being provided radially from the center. 小型ロケットの破裂による飛散物から観測者を守る保護板を有することを特徴とする請求項1記載の小型ロケット用発射台。Launch pad for small rockets according to claim 1 Symbol mounting and having a protective plate to protect the observer from debris by rupture of a small rocket. 上部板略中央に推力測定のための推力測定器を設けたことを特徴とする請求項1又は2項記載の小型ロケット用発射台。The launch pad for a small rocket according to claim 1 or 2, wherein a thrust measuring device for thrust measurement is provided at substantially the center of the upper plate.
JP2015117843A 2015-05-25 2015-05-25 Launch pad for small rocket Expired - Fee Related JP5927459B1 (en)

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Cited By (5)

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CN107154204A (en) * 2017-07-06 2017-09-12 中国科学技术馆 Rocket launching apparatus for demonstrating and demenstration method
CN109448527A (en) * 2018-11-12 2019-03-08 安徽徽煌教育科技有限公司 A kind of teenager's aviation knowledge expansion study spaceship lift-off practice device
CN110030874A (en) * 2019-03-29 2019-07-19 北京航天发射技术研究所 A kind of rocket swing rod that zero second swings back automatically that takes off removes receipts system
WO2021072828A1 (en) * 2019-10-14 2021-04-22 唐山维数科技有限公司 Launcher for simulating rocket launching
CN116538860A (en) * 2023-06-19 2023-08-04 北京天兵科技有限公司 Launching pad supporting arm structure and rocket launching pad device

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107154204A (en) * 2017-07-06 2017-09-12 中国科学技术馆 Rocket launching apparatus for demonstrating and demenstration method
CN107154204B (en) * 2017-07-06 2023-09-05 中国科学技术馆 Rocket launching demonstration device and demonstration method
CN109448527A (en) * 2018-11-12 2019-03-08 安徽徽煌教育科技有限公司 A kind of teenager's aviation knowledge expansion study spaceship lift-off practice device
CN109448527B (en) * 2018-11-12 2024-05-14 安徽徽煌教育科技有限公司 Spacecraft lift-off exercise device for teenager aviation knowledge expansion learning
CN110030874A (en) * 2019-03-29 2019-07-19 北京航天发射技术研究所 A kind of rocket swing rod that zero second swings back automatically that takes off removes receipts system
CN110030874B (en) * 2019-03-29 2021-06-11 北京航天发射技术研究所 Swing rod withdrawing system for automatic zero-second swinging of rocket during takeoff
WO2021072828A1 (en) * 2019-10-14 2021-04-22 唐山维数科技有限公司 Launcher for simulating rocket launching
CN116538860A (en) * 2023-06-19 2023-08-04 北京天兵科技有限公司 Launching pad supporting arm structure and rocket launching pad device

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