이안나 교수 연구실
article|
인용수 2
·2025
Plasma-assisted N2O/CH4 combustion in a rotating gliding arc thruster under ultra-lean conditions (Oxidizer-to-Fuel Ratio 5–1000)
Jeongrak Lee, S.S. Kim, Hanseong Jo, Anna Lee, Hongjae Kang
IF 5.8Aerospace Science and Technology
키워드
PropellantCombustionMonopropellantIgnition systemPropulsionFlammability limitArc (geometry)Spacecraft propulsion