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11 results on '"NAKATA, Daisuke"'

1. 自己加圧式ハイブリッドロケットの推力一定制御

Author

OKANO, Hiro, NAKATA, Daisuke, TADA, Takuya, EGUCHI, Hikaru, and UCHIUMI, Masaharu

Subjects
Throttling, Self pressurization, PID control, Hybrid rocket
Abstract

第5回ハイブリッドロケットシンポジウム(2023年2月14日. オンライン開催), 5th Hybrid Rocket Symposium(February 14, 2023. Online Meeting), 資料番号: SA6000186009, HR-2022-09

Published
2023

2. Development of Visualization System for Fuel Regression of Paraffin Wax in Acceleration Environments

Author

NEKI, Tomoya, OZAWA, Kohei, TSUBOI, Nobuyuki, NAKATA, Daisuke, UCHIUMI, Masaharu, and YASUDA, Kazuki

Subjects
Acceleration environment, Regression rate, Hybrid rocket, Wax fuel, Rocket sled
Abstract

第4回ハイブリッドロケットシンポジウム(2022年2月14日. オンライン開催), 4th Hybrid Rocket Symposium(February 14, 2022. Online Meeting), 資料番号: SA6000171015, HR-2021-15

Published
2022

3. PID Throttle Control of Self-pressurized Hybrid Rocket Engine

Author

YAMAGISHI, Kohki, NAKATA, Daisuke, YASUDA, Kazuki, SHIINA, Tatsuhiko, ANG, YiYong, TADA, Takuya, HASHIMOTO, Yuma, EGUCHI, Hikaru, and UCHIUMI, Masaharu

Subjects
PID controlle, Self-pressurization, Throttling, Hybrid Rocket, Thrust control
Abstract

第4回ハイブリッドロケットシンポジウム(2022年2月14日. オンライン開催), 4th Hybrid Rocket Symposium(February 14, 2022. Online Meeting), 資料番号: SA6000171010, HR-2021-10

Published
2022

4. Evaluation of Filling, Discharging and Flow Characteristics of Nitrous Oxide

Author

Yasuda, Kazuki, Nakata, Daisuke, and Uchiumi, Masaharu

Subjects
Self-pressurization, Nitrous oxide, Carbon dioxide, Hybrid rocket, Two-phase flow, Propellant supply system
Abstract

第2回ハイブリッドロケットシンポジウム（2019年7月11日-12日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, 2nd Hybrid Rocket Symposium (July 11-12, 2019. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000143011, レポート番号: HR-2019-010

Published
2019

5. Performance Characteristics of the 1kN-class Hybrid Rocket Engine

Author

Okada, Kugo, Nakata, Daisuke, Yasuda, Kazuki, and Uchiumi, Masaharu

Subjects
Rocket Noise, Nitrous Oxide, Hybrid Rocket, Rocket Sled
Abstract

平成30年度宇宙輸送シンポジウム（2019年1月17日-18日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2018 (January 17-18, 2019. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000136028, レポート番号: STCP-2018-028

Published
2019

6. Influence of Outside Temperature on Nitrous Oxide Self-Pressurized Discharging Characteristics

Author

Yasuda, Kazuki, Nakata, Daisuke, Uchiumi, Masaharu, Okada, Kugo, and Imai, Ryouji

Subjects
Self-pressurized tank, Nitrous oxide, Cold flow test, Hybrid rocket, Two-phase flow
Abstract

第1回ハイブリッドロケットシンポジウム（2018年6月28日-29日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, 1st Hybrid Rocket Symposium (June 28-29, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000126008, レポート番号: HR-2018-007

Published
2018

7. Operation of a Rocket Sled using Hybrid Rocket Engines

Author

Nakata, Daisuke, Yasuda, Kazuki, Okada, Kugo, Higuchi, Ken, Katsumata, Nobuhisa, and Uchiumi, Masaharu

Subjects
Hybrid Rocket, Rocket Sled, Ignition, Clustering
Abstract

第1回ハイブリッドロケットシンポジウム（2018年6月28日-29日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, 1st Hybrid Rocket Symposium (June 28-29, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000126011, レポート番号: HR-2018-010

Published
2018

8. Experimental Study on the Ignition Delay of Hybrid Rockets

Author

Nakata, Daisuke, Muhammad, Hafeez, Tanatsugu, Nobuhiro, Higashino, Kazuyuki, and Hirota, Mitsutomo

Subjects
Ignition Delay, Hybrid Rocket, Flame Spread Velocity
Abstract

平成25年度宇宙輸送シンポジウム（2014年1月16日-17日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2013 (January 16-17, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000016044, レポート番号: STCP-2013-044

Published
2014

9. Faster and Larger Acceleration-G Rocket Sled System

Author

Nakata, Daisuke, Nishine, Kenji, Tateoke, Kaoru, Muhammad, Nabil, Tanatsugu, Nobuhiro, and Higashino, Kazuyuki

Subjects
High Speed Test Track, anti-G test, Hybrid Rocket, Rocket Sled, Drag
Abstract

平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, High Speed Rocket Sled Track Facility is in use from 2009 in Hokkaido prefecture. Fundamental study was carried out in order to extend its capability of maximum speed and acceleration G condition. Structure design guideline was established and verified by static load test. Running profile estimation tool was developed taking careful treatment especially in air drag and water drag calculation. Resultantly 405 km/h as its top speed was recorded within the coast distance of 275 m. The sled felt 7 G during deceleration phase and no damage was recognized in its structure or electronic equipment., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856057, レポート番号: STCP-2012-057

Published
2013

10. Basic Technology on the High Speed Test Track

Author

Nakata, Daisuke, Yajima, Jun, Nishine, Kenji, Moriki, Takato, Muhammadfakhlullah, Higashino, Kazuyuki, and Tanatsugu, Nobuhiro

Subjects
Drag Coefficient, High Speed Test Track, Hybrid Rocket, Rocket Sled, Aerodynamic balance
Abstract

平成23年度宇宙輸送シンポジウム（2012年1月19日-20日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)（ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2011 (January 19-20, 2012. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000003063, レポート番号: STCP-2011-063

Published
2012

11. Rocket Sled with Hybrid Rocke

Author

Nakata, Daisuke, Kozu, Ami, Yjima, Jun, Nishine, Kenji, Higashino, Kazuyuki, and Tanatsugu, Nobuhiro

Subjects
Hybrid Rocket, Water Resistance, Rocket Sled, Aerodynamic Measurement
Abstract

平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Rocket sled is well known device that enables us to measure aerodynamic effect in full-scale model. In United States, rocket sleds have been utilized for the validation experiments of many practical aircrafts and spacecrafts. Muroran Institute of Technology constructed 1.4 m in width, 300 m in length test track and started the operation of full-scale rocket sled. As an acceleration system, tandem hybrid rockets are used. An optimum deceleration system within the limited track length was attempted by stepwise water braking system. Frequent reconsideration of operation procedure reduced the turn around time to 2 hour with 4 people., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065073015

Published
2011

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