Folgen
Landon Kamps
Landon Kamps
Letara Ltd. and Hokkaido University
Bestätigte E-Mail-Adresse bei eng.hokudai.ac.jp
Titel
Zitiert von
Zitiert von
Jahr
Method for determining nozzle-throat-erosion history in hybrid rockets
L Kamps, Y Saito, R Kawabata, M Wakita, T Totani, Y Takahashi, ...
Journal of propulsion and power 33 (6), 1369-1377, 2017
392017
Investigation of graphite nozzle erosion in hybrid rockets using oxygen/high-density polyethylene
L Kamps, S Hirai, K Sakurai, T Viscor, Y Saito, R Guan, H Isochi, N Adachi, ...
Journal of propulsion and power 36 (3), 423-434, 2020
272020
Hybrid rockets as post-boost stages and kick motors
L Kamps, S Hirai, H Nagata
Aerospace 8 (9), 253, 2021
252021
Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation
L Kamps, K Sakurai, Y Saito, H Nagata
Aerospace 6 (4), 45, 2019
242019
The accuracy of reconstruction techniques for determining hybrid rocket fuel regression rate
Y Saito, LT Kamps, K Komizu, D Bianchi, F Nasuti, H Nagata
2018 Joint Propulsion Conference, 4923, 2018
202018
Numerical analysis of nozzle erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, L Kamps, H Nagata
Journal of Propulsion and Power 38 (3), 389-409, 2022
182022
Numerical and experimental investigation of nozzle thermochemical erosion in hybrid rockets
D Bianchi, LT Kamps, F Nasuti, H Nagata
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4640, 2017
142017
Large-scale CAMUI type hybrid rocket motor scaling, modeling, and test results
T Viscor, L Kamps, K Yonekura, H Isochi, H Nagata
Aerospace 9 (1), 1, 2021
122021
Fuel regression characteristics of axial-injection end-burning hybrid rocket using nitrous oxide
R Okuda, K Komizu, A Tsuji, T Miwa, M Fukada, S Yokobori, K Soeda, ...
Journal of propulsion and power 38 (5), 759-770, 2022
112022
Fuel regression characteristics in hybrid rockets using nitrous oxide/high-density polyethylene
S Ito, L Kamps, H Nagata
Journal of propulsion and power 37 (2), 342-348, 2021
112021
Evaluation of the Thermal Onset of Graphite Nozzle Erosion
S Ito, LT Kamps, S Yoshimal, H Nagata
AIAA Propulsion and Energy 2020 Forum, 3755, 2020
112020
Development of N2O/HDPE hybrid rocket for microsatellite propulsion
L Kamps, P Molas-Roca, E Uchiyama, T Takanashi, H Nagata
70th International Astronautical Congress (IAC-19), Washington DC, United …, 2019
112019
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using N2O/HDPE
LT Kamps, K Sakurai, K Ozawa, H Nagata
AIAA Propulsion and Energy 2019 Forum, 4264, 2019
102019
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4
LT Kamps, S Hirai, K Sakurai, T Viscor, Y Saito, R Guan, H Isochi, ...
2018 Joint Propulsion Conference, 4531, 2018
82018
GEO-X (GEOspace x-ray imager)
Y Ezoe, R Funase, H Nagata, Y Miyoshi, S Kasahara, H Nakajima, ...
Space telescopes and instrumentation 2020: Ultraviolet to gamma ray 11444 …, 2020
72020
One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket
G Gallo, L Kamps, S Hirai, C Carmicino, H Nagata
Acta Astronautica 210, 176-196, 2023
62023
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, LT Kamps, H Nagata
AIAA Propulsion and Energy 2020 Forum, 3767, 2020
62020
Fuel regression characteristics of CAMUI type hybrid rocket using nitrous oxide
Y Nobuhara, LT Kamps, H Nagata
AIAA Propulsion and Energy 2021 Forum, 3521, 2021
52021
Development of safe, low-cost, re-ignitable rocket ignition system
S Hirai, LT Kamps, H Nagata
AIAA Propulsion and Energy 2021 Forum, 3509, 2021
52021
GEO-X (GEOspace x-ray imager)
Y Ezoe, R Funase, H Nagata, Y Miyoshi, H Nakajima, I Mitsuishi, ...
Space Telescopes and Instrumentation 2022: Ultraviolet to Gamma Ray 12181 …, 2022
42022
Das System kann den Vorgang jetzt nicht ausführen. Versuchen Sie es später erneut.
Artikel 1–20