1 김선진, "친환경 추진제인 과산화수소와 액체메탄의 활용 역사와 연구 동향" 한국추진공학회 14 (14): 46-58, 2010
2 정기정, "우주개발을 위한 차세대 메탄엔진 개발 동향" 한국항공우주학회 45 (45): 558-565, 2017
3 전준수, "가스메탄/액체산소를 추진제로 하는 단일 인젝터 설계 및 실험적 검증" 대한기계학회 37 (37): 275-283, 2013
4 "UBC Rocket"
5 "Rocket Prorulsion Combustion Laboratory"
6 Bryner, E, "Rocket Development and Testing Capabilities at Embry-Riddle Aeronautical University – Prescott AZ campus" 2019
7 Pourpoint, T, "Propulsion Test Facilities at the Purdue University Maurice J.Zucrow Laboratories" 2007
8 Simontacchi, P, "Prometheus: Precursor of new low-cost rocket engine family" 2019
9 Iannetti, A, "Prometheus, a LOX/LCH4 Reusable Rocket Engine" 2017
10 Morehead, R.L, "Project Morpheus Main Engine Development and Preliminary Flight Testing" 2011
1 김선진, "친환경 추진제인 과산화수소와 액체메탄의 활용 역사와 연구 동향" 한국추진공학회 14 (14): 46-58, 2010
2 정기정, "우주개발을 위한 차세대 메탄엔진 개발 동향" 한국항공우주학회 45 (45): 558-565, 2017
3 전준수, "가스메탄/액체산소를 추진제로 하는 단일 인젝터 설계 및 실험적 검증" 대한기계학회 37 (37): 275-283, 2013
4 "UBC Rocket"
5 "Rocket Prorulsion Combustion Laboratory"
6 Bryner, E, "Rocket Development and Testing Capabilities at Embry-Riddle Aeronautical University – Prescott AZ campus" 2019
7 Pourpoint, T, "Propulsion Test Facilities at the Purdue University Maurice J.Zucrow Laboratories" 2007
8 Simontacchi, P, "Prometheus: Precursor of new low-cost rocket engine family" 2019
9 Iannetti, A, "Prometheus, a LOX/LCH4 Reusable Rocket Engine" 2017
10 Morehead, R.L, "Project Morpheus Main Engine Development and Preliminary Flight Testing" 2011
11 Huzel, D. K, "Progress in Astronautics and Aeronautics" 199
12 Kang, C.W, "Preliminary Hot-firing Tests of 400 N Class Methane Engine Thrust Chamber" 2020
13 Kim, D. H, "Performance and Ignition Characteristic of a Coaxial Swirl Injector using LOX-GCH4 Propellant" 72-76, 2010
14 Melcher, J, "Liquid Oxygen/Liquid Methane Test Results of the RS-18 Lunar Ascent Engine at Simulated Altitude Conditions at NASA White Sands Test Facility" 2012
15 Cho, Y.H, "Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG" 2004
16 Klem, M. D, "Guidelines for Combustion Stability Specifications and Verification Procedures for Liquid Propellant Rocket Engines" CPIA 1997
17 Kim, K.H, "Development of ‘chase-10’ Liquid Rocket Engine having 10tf thrust using lox & lng (methane)" 2006
18 Rudnykh, M, "Development of LM10-MIRA LOX/LNG expander cycle demonstrator engine" 126 : 364-374, 2016
19 Bauer, C, "Design and commission of a mobile GOX/GCH4 rocket combustion test bed for education and collegiate research" 2013
20 Melcher, J.C, "Combustion Stability Characterisrics of the Project Morpheus Liquid Oxygen/Liquid Methane Main Engine" 2014
21 Asakawa, H, "Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials" Springer 463-487, 2017
22 Ommi, F, "A Practical Scenario for Cold and Hot-Fire Test of a Liquid Subscale Engine with Single Swirl Double Base Injector" 3 (3): 84-100, 2015
23 김민철, "200 N급 GCH4/LOx 소형로켓엔진의 형상설계와 성능시험평가 (Part II: 정상상태 지상연소시험)" 한국추진공학회 24 (24): 9-16, 2020
24 김영진, "200 N급 GCH4/LOx 소형로켓엔진의 형상설계와 성능시험평가 (Part I: 예비설계와 시험장치)" 한국추진공학회 24 (24): 1-8, 2020