1 김정진 ; 오석진 ; 허준영 ; 이도형, "공압시험용 플러그 노즐의 핀틀 형상 및 작동압력에 따른 유동 특성 분석" 한국추진공학회 23 (23): 28-34, 2019
2 Jeong, K. Y, "Thrust Characteristics of Through-type Pintle Nozzles with Large Scale Seperation Flow" 32-38, 2014
3 Ha, D.S, "Research Trends in Propulsion Technology for Divert and Attitude Control System" 353-357, 2017
4 Park, H. J, "Numerical Study on Dynamic Characteristics of Pintle Nozzle for Variant Thrust" 213-217, 2011
5 Sayles, D.C, "Development of Test Motors for Advanced Controllable Propellants" 12 (12): 174-178, 1975
6 Nijanthan, M, "Conceptual Design and Shape Optimization of a Pintle Nozzle for Controllable Thrust Propulsion and Steering" 2017
7 김정진, "Analysis of the Characteristics of an Aerospike Pintle Nozzle in terms of Stroke and Operating Pressure" 항공우주시스템공학회 14 (14): 1-9, 2020
8 Ervin, W.D, "Altitude Test of the Aerojet Modified Heavyweight Full-Scale Controllable Solid-Propellant Rocket Motor(CSRM-4)" 1973
9 Ravnan, S, "Advantage of a Supersonic Split line nozzle over a submerged movable nozzle" Delft University of Technology 2021
10 Sayles, D.C, "Advanced Pintle-Controlled Motor with Thrust Vector Control, SAE Transactions 710619-710867, Vol. 80, Section 4"
1 김정진 ; 오석진 ; 허준영 ; 이도형, "공압시험용 플러그 노즐의 핀틀 형상 및 작동압력에 따른 유동 특성 분석" 한국추진공학회 23 (23): 28-34, 2019
2 Jeong, K. Y, "Thrust Characteristics of Through-type Pintle Nozzles with Large Scale Seperation Flow" 32-38, 2014
3 Ha, D.S, "Research Trends in Propulsion Technology for Divert and Attitude Control System" 353-357, 2017
4 Park, H. J, "Numerical Study on Dynamic Characteristics of Pintle Nozzle for Variant Thrust" 213-217, 2011
5 Sayles, D.C, "Development of Test Motors for Advanced Controllable Propellants" 12 (12): 174-178, 1975
6 Nijanthan, M, "Conceptual Design and Shape Optimization of a Pintle Nozzle for Controllable Thrust Propulsion and Steering" 2017
7 김정진, "Analysis of the Characteristics of an Aerospike Pintle Nozzle in terms of Stroke and Operating Pressure" 항공우주시스템공학회 14 (14): 1-9, 2020
8 Ervin, W.D, "Altitude Test of the Aerojet Modified Heavyweight Full-Scale Controllable Solid-Propellant Rocket Motor(CSRM-4)" 1973
9 Ravnan, S, "Advantage of a Supersonic Split line nozzle over a submerged movable nozzle" Delft University of Technology 2021
10 Sayles, D.C, "Advanced Pintle-Controlled Motor with Thrust Vector Control, SAE Transactions 710619-710867, Vol. 80, Section 4"