Browse > Article

Design of PSD Performance Test System  

고광웅 (한국과학기술원 기계공학과)
정동운 (한국과학기술원 기계공학과)
이한주 (한국항공우주연구원 추진기관그룹)
이상용 (한국과학기술원 기계공학과)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.7, no.4, 2003 , pp. 10-18 More about this Journal
Abstract
In the present study, several different types of PSD performance test systems were reviewed. Basically there are two methods to pulsate the system; whole-feeding-system pulsation and working-fluid pulsation. The latter method adopts either a piston-type pulsator or a restrict-type pulsator The working-fluid pulsation using a restrict-type pulsator was considered to be the most appropriate experimental system to study the effects of the primary parameters, and a practical design of the system was proposed.
Keywords
POGO; PSD; Whole-feeding-system Pulsation; Working-fluid Pulsation; Piston-type; Restrict-type;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 R. Fenwick, J. H. Jones, R. E. Jewell, 'Space Shuttle Main Engine (SSME) Pogo Testing and Results,' The Shock and Vibration Bulletin, No. 52, Pt. 2, 1982, pp. 1-20
2 L. W. S. Norquist, J. P. Marcus, D. A. Ruscio, 'Development of Close-Coupled Accumulators for Suppressing Missile Longitudinal Oscillations (POGO),' AIAA Paper No. 69-547
3 H. H. Doiron, 'Space Shuttle Pogo Prevention,' NASA-TM-79526
4 'NASa Space Vehicle Design Criteria Liquid Rocket Lines, Bellows, Flexible Hoses, And Filters,' NASA-SP 8123
5 Sheldon Rubin, 'Longitudinal Instability of Liquid Rockets due to Propulsion Feedback(Pogo),' J. Spacecraft, Vol. 3, No. 8, 1966, pp. 1188-1195   DOI
6 오승협 등, 우주발사체사업 보고서, 항공우주연구원, 2003
7 'Measurement of Fluid Flow by Means of Orifice Plate, Nozzle, and Venturi Tubes, Inserted in Circular Cross Section Conduits Running Full,' Int. Organ. Stand. Rep. DIS-5617, Geneva, April 1976
8 고광웅, 이한주, 정동운, 이상용, 'POGO와 PSD의 소개', 한국추진공학회지, 제7권 제4호. 2003. pp. 1-9