KAMPS LANDON KAMPS LANDON

Researcher Number	70869502
Other IDs
Affiliation (based on the past Project Information) *help	2020 – 2022: 北海道大学, 工学研究院, 特任助教
Review Section/Research Field	Principal Investigator Basic Section 24010:Aerospace engineering-related Except Principal Investigator Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields / Transformative Research Areas, Section (II)
Keywords	Principal Investigator 黒鉛 / 再生冷却 / ノズル浸食 / ハイブリッドロケット Except Principal Investigator ロケット / 宇宙推進 / ハイブリッドロケット / 光造形 / 3D印刷 / 端面燃焼 … More / 固体燃焼 / 端面燃焼式 / 推進 / 宇宙 / 地上燃焼実験 / 軌道変換 / 小型宇宙機 / キックモータ / ノズル浸食 / 軌道変換ロケット / 小型相乗り宇宙機 Less

液体酸素を用いる端面燃焼式ハイブリッドロケットの実証研究
- Principal Investigator
  
  永田晴紀
- Project Period (FY)
  2022 – 2025
- Research Category
  
  Grant-in-Aid for Scientific Research (A)
- Review Section
  
  Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
- Research Institution
  Hokkaido University
Demonstration of Graphite Nozzle Erosion Suppression in Hybrid Rockets Through Regenerative CoolingPrincipal Investigator
- Principal Investigator
  
  KAMPS LANDON
- Project Period (FY)
  2020 – 2022
- Research Category
  
  Grant-in-Aid for Early-Career Scientists
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Hokkaido University
Development of a Hybrid Kick Motor to Provide Innovative Orbit-Transfer Capabilities for Micro-Spaceproves
- Principal Investigator
  
  Nagata Harunori
- Project Period (FY)
  2020 – 2022
- Research Category
  
  Grant-in-Aid for Transformative Research Areas (B)
- Review Section
  
  Transformative Research Areas, Section (II)
- Research Institution
  Hokkaido University

All 2023 2022 2021 2020

All Journal Article Presentation

[Journal Article] Regenerative Cooling of Graphite Nozzles for Throat Erosion Suppression2023
- Author(s)
  Kojima Hiroki、Kamps Landon T.、Nobuhara Yuki、Gallo Giuseppe、Nagata Harunori
- Journal Title
  
  AIAA SciTech
  
  Volume: -
- DOI
  10.2514/6.2023-1830
- Peer Reviewed / Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-20K14946
[Journal Article] Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide2022
- Author(s)
  Okuda Ryota、Komizu Kodai、Tsuji Ayumu、Miwa Takumi、Fukada Mai、Yokobori Shuichi、Soeda Kentaro、Kamps Landon、Nagata Harunori
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 38 Issue: 5 Pages: 759-770
- DOI
  10.2514/1.b38318
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-22H00240
[Journal Article] Fuel Regression Characteristics of CAMUI type Hybrid Rocket Using Nitrous Oxide2021
- Author(s)
  Nobuhara Yuki、Kamps Landon T.、Nagata Harunori
- Journal Title
  
  AIAA Propulsion and Energy Forum
  
  Volume: -
- DOI
  10.2514/6.2021-3521
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747
[Journal Article] Development of safe, low-cost, re-ignitable rocket ignition system2021
- Author(s)
  Hirai Shota、Kamps Landon T.、Nagata Harunori
- Journal Title
  
  AIAA Propulsion and Energy Forum
  
  Volume: -
- DOI
  10.2514/6.2021-3509
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747
[Journal Article] Experimental Investigation of N<sub>2</sub>O/GOX Compounds as Hybrid Rocket Oxidizers2021
- Author(s)
  Inoue Hajime、Kamps Landon T.、Cadou Christopher P.、Inoue Shota、Takada Yusuke、Nobuhara Yuki、Nagata Harunori
- Journal Title
  
  AIAA Propulsion and Energy Forum
  
  Volume: -
- DOI
  10.2514/6.2021-3520
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747
[Journal Article] Hybrid Rockets as Post-Boost Stages and Kick Motors2021
- Author(s)
  Kamps Landon、Hirai Shota、Nagata Harunori
- Journal Title
  
  Aerospace
  
  Volume: 8 Issue: 9 Pages: 253-253
- DOI
  10.3390/aerospace8090253
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747, KAKENHI-PROJECT-19H02336
[Journal Article] Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene2021
- Author(s)
  Ito, S., Kamps, L., and Nagata, H.
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 37 Issue: 2 Pages: 342-348
- DOI
  10.2514/1.b37875
- NAID
  120007041995
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747, KAKENHI-PROJECT-19H02336
[Journal Article] Ignition and flame-holding characteristics of 60wt% hydrogen peroxide in a CAMUI-type hybrid rocket fuel2021
- Author(s)
  Takada Yusuke、Iwanaga Kodai、Inoue Hajime、Inoue Shota、Wakita Masashi、Kamps Landon T.、Sahara Hironori、Iizuka Toshiaki、Nagata Harunori
- Journal Title
  
  AIAA Propulsion and Energy Forum
  
  Volume: - Pages: 0-0
- DOI
  10.2514/6.2021-3511
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747, KAKENHI-PROJECT-19H02336
[Journal Article] Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments2021
- Author(s)
  Bianchi Daniele、Migliorino Mario Tindaro、Rotondi Marco、Kamps Landon、Nagata Harunori
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: Online Issue: 3 Pages: 1-22
- DOI
  10.2514/1.b38547
- Peer Reviewed / Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-19H02336, KAKENHI-PROJECT-20K14946, KAKENHI-PLANNED-20H05747
[Presentation] Application of Low Concentration Hydrogen Peroxide for Hybrid Rocket Propulsion System for Small Spacecraft2023
- Author(s)
  Masashi Wakita, Yusuke Takada, Kodai Iwanaga, Toshiaki Iizuka, Hironori Sahara, Landon T. Kamps and Harunori Nagata
- Organizer
  AIAA SCITECH 2023 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Nitrous Oxide2023
- Author(s)
  Giuseppe Gallo, Landon T. Kamps, Shota Hirai, Carmine Carmicino and Harunori Nagata
- Organizer
  AIAA SCITECH 2023 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Demonstration of Axial-Injection End-Burning Hybrid Rocket using FDM 3D Printer2023
- Author(s)
  Hirai Shota、Kamps Landon T.、Nobuhara Yuki、Nagata Harunori
- Organizer
  AIAA SCITECH 2023 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] Combustion Characteristics of Axial-Injection End-Burning Hybrid Rockets using Liquid Oxygen2023
- Author(s)
  Suzuki, S., Minami, K., Son, s., Fukada, M., Kamps, L., Wakita, M., and Nagata, H.
- Organizer
  74th International Astronautical Congress
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] Regenerative Cooling of Graphite Nozzles for Throat Erosion Suppression2023
- Author(s)
  Hiroki Kojima, Landon T. Kamps, Yuki Nobuhara, Giuseppe Gallo and Harunori Nagata
- Organizer
  AIAA SCITECH 2023 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Liquid Nitrous Oxide2022
- Author(s)
  Giuseppe Gallo, Landon T. Kamps, Shota Hirai, Carmine Carmicino and Harunori Nagata
- Organizer
  International Astronautical Congress
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Safe and Low Voltage Rocket Ignition System using electrically conductive plastics2022
- Author(s)
  Shota Hirai, Yownin A. Leung, Landon T. Kamps and Harunori Nagata
- Organizer
  AIAA AVIATION 2022 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Fuel regression characteristics of axial-injection end-burning hybrid rockets using Nitrous Oxide2022
- Author(s)
  Mai Fukada, Hiroki Hayasaka, Sho Suzuki, Landon Kamps, Masashi Wakita, Harunori Nagata
- Organizer
  73rd International Astronautical Congress 2022
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] One-Dimensional Model for the Study of Helical Cooling Channels Based on Cryogenic Oxygen in Hybrid Rocket Engines2022
- Author(s)
  Giuseppe Gallo, Shota Hirai, Landon Kamps, Harunori Nagata
- Organizer
  19th International Conference on Flow Dynamics
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-20K14946
[Presentation] Progress Towards Graphite Nozzle Cooling for Throat Erosion Suppression2022
- Author(s)
  Hiroki Kojima, Landon T. Kamps, Yuki Nobuhara, Harunori Nagata, Thomas Valembois and Camille Cottenot
- Organizer
  AIAA AVIATION 2022 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Regenerative Cooling Concept for Thermal Management of Graphite Nozzle Throat2020
- Author(s)
  Landon Kamps, Seiji Ito, Harunori Nagata
- Organizer
  17th International Conference on Flow Dynamics（国際学会）
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-20K14946
[Presentation] ハイブリッドロケットの点火器に関する研究2020
- Author(s)
  池田華子，ランドンケンプス，永田晴紀
- Organizer
  第58回燃焼シンポジウム
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Evaluation of the Thermal Onset of Graphite Nozzle Erosion2020
- Author(s)
  Seiji Ito, Landon Kamps, Satoshi Yoshimaru, Harunori Nagata
- Organizer
  AIAA Propulsion and Energy Forum（国際学会）
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-20K14946
[Presentation] ハイブリッドロケットの軸方向後燃料退速度に関する３Dスキャナを用いた研究2020
- Author(s)
  奥田晃崇，Landon Kamps，伊藤聖司，影山理沙，Tor Viscor，井上翔太，池田華子，高田祐亮，脇田督司，永田晴紀
- Organizer
  第58回燃焼シンポジウム
- Data Source
  KAKENHI-PLANNED-20H05747

1. Nagata Harunori (40281787)

# of Collaborated Projects: 2 results

# of Collaborated Products: 19 results
2. 脇田督司 (80451441)

# of Collaborated Projects: 2 results

# of Collaborated Products: 5 results
3. 添田建太郎 (30795050)

# of Collaborated Projects: 1 results

# of Collaborated Products: 1 results

KAMPS LANDON KAMPS LANDON

Research Projects

Research Products

Co-Researchers

液体酸素を用いる端面燃焼式ハイブリッドロケットの実証研究

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Demonstration of Graphite Nozzle Erosion Suppression in Hybrid Rockets Through Regenerative CoolingPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Development of a Hybrid Kick Motor to Provide Innovative Orbit-Transfer Capabilities for Micro-Spaceproves

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

[Journal Article] Regenerative Cooling of Graphite Nozzles for Throat Erosion Suppression2023

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide2022

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Fuel Regression Characteristics of CAMUI type Hybrid Rocket Using Nitrous Oxide2021

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Development of safe, low-cost, re-ignitable rocket ignition system2021

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Experimental Investigation of N<sub>2</sub>O/GOX Compounds as Hybrid Rocket Oxidizers2021

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Hybrid Rockets as Post-Boost Stages and Kick Motors2021

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene2021

Author(s)

Journal Title

DOI

NAID

Data Source

[Journal Article] Ignition and flame-holding characteristics of 60wt% hydrogen peroxide in a CAMUI-type hybrid rocket fuel2021

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments2021

Author(s)

Journal Title

DOI

Data Source

[Presentation] Application of Low Concentration Hydrogen Peroxide for Hybrid Rocket Propulsion System for Small Spacecraft2023

Author(s)

Organizer

Data Source

[Presentation] Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Nitrous Oxide2023

Author(s)

Organizer

Data Source

[Presentation] Demonstration of Axial-Injection End-Burning Hybrid Rocket using FDM 3D Printer2023

Author(s)

Organizer

Data Source