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Hiromasa Kamezawa
Hiromasa Kamezawa
Automatic Flight Control System Lead Engineer at Honda Aircraft Company
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Title
Cited by
Cited by
Year
Design of a novel hypersonic inflatable aerodynamic decelerator for mars entry, descent, and landing
N Skolnik, H Kamezawa, L Li, GA Rossman, B Sforzo, RD Braun
AIAA Atmospheric Flight Mechanics Conference, 0469, 2017
142017
Approximate convective heat flux calculation methods for hypersonic vehicles
H Kamezawa, SM Ruffin
2018 AIAA Aerospace Sciences Meeting, 0244, 2018
22018
Design Study on Booster Vehicles of a TSTO RLV with RBCC Engines Part2: Waverider Configuration
N Morita
JSASS-2015-4454, 0
2
Design Study on Booster Vehicles of a TSTO RLV with RBCC Engines Part1: Lifting Body Configuration
N Morita
JSASS-2015-4453, 0
2
Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing
L Li, G Rossman, N Skolnik, H Kamezawa, A Longo, RD Braun, B Sforzo
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Articles 1–5