Výsledky vyhledávání - "FURUTA, Toshiyasu"

Experimental Research on the Heat Insulation Coating of SSR

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):613-621

Many fundamental testings for the heat insulation coating of SSR were done in our laboratory. Some results of our testings are available in the actual rocket. This report describes also about some results of experimental research, which are not used

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::110103fdce28af12eccdce765d20e178
http://id.nii.ac.jp/1696/00031819/

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Heat-resisting Characteristic of Graphite Penetrated by Silicone Oil

Autor: IKEDA, Ken, FURUTA, Toshiyasu, MIURA, Koryo, SAKAMAKI, Masamori

Publikováno v: 東京大学航空研究所集報. 4(1):1-6

グラファイトは固体ロケットモータのノズルとして使用されるが,その耐熱特性の改善のためにシリコーンオイルをグラファイトの試験片に真空槽で含浸させ,酸素-アセチレンバーナで試�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::06ff4b8e60ed2fba9896a2d5bd95695f
http://id.nii.ac.jp/1696/00035212/

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On the Strength of the Structural Parts of SSR-Rocket

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):585-602

This report describes the details of the fundamental testing and the strength test of the actual recket body. The contents are a) Calculation of the bending strength and stiffness of the rocket body, b) Measurement of stress and stiffness of the bend

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3ec7f08ef8c2c6322cd7f45727c4e2ca
http://id.nii.ac.jp/1696/00031816/

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On the Ablation Characteristics of the Laminated Foils

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学航空研究所集報. 2(7):428-432

ロケットボディの外皮を空力加熱から守るために,しばしばアブレーション材料が用いられ,また,固型推薬ロケットエンジンのシリンダの内側にもこれらを用いることがある.アブレーショ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::df950910f27de8e213b431666fcbf637
http://id.nii.ac.jp/1696/00035123/

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On the Insulation Effect of Phenolic Resin

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 1(3_A):103-108

ロケットのエンジンやボディには,しばしば耐熱塗料が用いられる.このようなコーティングに対する要求としては,アブレーション効果のよいことと同時に,加熱中にも母材の金属などに対

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a1495168555ea818b5f9c26a0a979770
http://id.nii.ac.jp/1696/00031469/

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On the structure of the Nozzle of the Motor of SSR-Rocket

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):580-584

The structure of the nozzle of the motor of SSR is shown in Fig. 2. Alalloy is capable to be replaced for the steel part in a common conventional design, owing to the good effect of insulator between the graphite of the throat and the Al-alloy casing

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e80ffbd8a80c4718d0fd9562ce802f16
http://id.nii.ac.jp/1696/00031815/

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Rossibility of Structural Improvement of SSR-Rocket

Autor: IKEDA, Ken, TOMITA, Bunji, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):622-626

The small test rocket SSR, Which reached the altitude 25.8km in the latest flying test, is still possible to be improved from the structural point of view. From the results of the ground tests, the weight of some structual parts can be reduced and th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::cce2b81fa3be9356fcc3689e80fabb6c
http://id.nii.ac.jp/1696/00031820/

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On the Details of the Structure of SSR

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKi, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):610-612

Main principles of the structural design of SSR and its somewhat detailed points are already reported in other papers written by the authors. So in this paper we report about the details especially concerning with the end structures of the motor; for

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b4278c7afab031a295cc5d2299271d8c
http://id.nii.ac.jp/1696/00031818/

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On the Heat Insulation Coating of SSR-Rocket Motor

Autor: IKEDA, Ken, FURUTA, Toshiyasu, SAKAMAKI, Masamori

Publikováno v: 東京大学宇宙航空研究所報告. 2(2_B):677-679

Main requirements for a insulation coating inside the cylinder wall of solid propellant rocket motor are that it must have a) Good heat insulation effect, b) Good bonding to the cylinder wall, c) Easiness of painting operation. We used, as the insula

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1c55655a1f6820ea0505d27e56b514b0
http://id.nii.ac.jp/1696/00031824/

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