• Title/Summary/Keyword: Stage Separation

Search Result 410, Processing Time 0.027 seconds

Pyroshock and Vibration Characteristics of PEEK Washer Shock Absorbers (PEEK 와셔를 적용한 충격저감장치의 파이로 충격 및 진동 특성)

  • Youn, Se-Hyun;Jang, Young-Soon;Han, Jae-Hung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.36 no.3
    • /
    • pp.285-290
    • /
    • 2008
  • Pyrotechnic shock or pyroshock is characterized as a transient vibration phenomena which shows large acceleration and high frequency range up to 10kHz during the operation of separation devices where explosives are used. During the flight of a launch vehicle, pyro-shock is mainly generated at several events such as satellite separation, fairing separation and stage separation. In this paper, characteristics of pyroshock are introduced briefly, and PEEK washer shock absorber is applied for the reduction of pyroshock in the high frequency range. With some electronic devices, reduction characteristic of pyroshock using washer type shock absorber are studied. Random vibration tests are also performed for the verification of vibrational characteristics.

Center-of-Gravity Effect on Supersonic Separation from the Mother Plane (무게중심 변화에 따른 초음속 공중발사 로켓의 모선분리 연구)

  • Ji Young-Moo;Lee Jae-Woo;Byun Yung-Hwan;Park Jun-Sang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2006.05a
    • /
    • pp.36-40
    • /
    • 2006
  • An analysis is made of flow and rocket motion during a supersonic separation stage of air-launching rocket(ALR) from the mother plane. Three-dimensional compressible Navier-Stokes equations is numerically solved to analyze the steady/unsteady flow field around the rocket which is being separated from the mother plane configuration(F-4E Phantom). The simulation results clearly demonstrate the effect of shock-expansion wave interaction between the rocket and the mother plane. To predict the behavior of the ALR according to the change of the C.G., three cases of numerical analysis are performed. As a result, a design-guideline of supersonic air-launching rocket for the safe separation is proposed.

  • PDF

THE PROCESS OF PLAYTHERAPY OF A CHILD WITH ELECTIVE MUTISM (선택적 함구증을 보인 6세아동의 놀이치료)

  • Kwak, Young-Sook
    • Journal of the Korean Academy of Child and Adolescent Psychiatry
    • /
    • v.3 no.1
    • /
    • pp.138-146
    • /
    • 1992
  • The study presented the experience of playtherapy of a 6-yr old girl with elective mutism and attempted to understand her psychopathology and formulated her psychodynamic which was expressed though the therapeutic process of playtherapy in the viewpoint of developmental model. Therapist's attitude was nondirective and supportive. Main theme of her play, fantasy and art was separation anxiety and abandonment fear as the result of continued psychic traumas such as separation from her grandmother and physical abuse by her father and mother etc. So she couldn't achieve developmental tasks such as autonomy and separation individuation and became generally inhibited and selectively mute. The process of play therapy was summarized and coceptualized as her successful progress through sequential developmental phases within the therapeutic relation ship. By reexperiencing this developmental process, she could accomplish her autonomy and separation individuation and developed to oedipal stage and successfully resolve oedipal conflict.

  • PDF

Audio Watermarking Using Independent Component Analysis

  • Seok, Jong-Won
    • Journal of information and communication convergence engineering
    • /
    • v.10 no.2
    • /
    • pp.175-180
    • /
    • 2012
  • This paper presents a blind watermark detection scheme for an additive watermark embedding model. The proposed estimation-correlation-based watermark detector first estimates the embedded watermark by exploiting non-Gaussian of the real-world audio signal and the mutual independence between the host-signal and the embedded watermark and then a correlation-based detector is used to determine the presence or the absence of the watermark. For watermark estimation, blind source separation (BSS) based on independent component analysis (ICA) is used. Low watermark-to-signal ratio (WSR) is one of the limitations of blind detection with the additive embedding model. The proposed detector uses two-stage processing to improve the WSR at the blind detector; the first stage removes the audio spectrum from the watermarked audio signal using linear predictive (LP) filtering and the second stage uses the resulting residue from the LP filtering stage to estimate the embedded watermark using BSS based on ICA. Simulation results show that the proposed detector performs significantly better than existing estimation-correlationbased detection schemes.

A Study on the Separation Minima for Urban Air Mobility in Low-Density Operation Environments (저밀도 운용 환경에서의 도심항공교통 분리 기준에 관한 연구)

  • Hyoseok Chang;Dohyun Kim;Jaewoo Kim;Daniel Kim;Heeduk Cho
    • Journal of Advanced Navigation Technology
    • /
    • v.27 no.6
    • /
    • pp.710-715
    • /
    • 2023
  • Urbanization brings many challenges such as traffic, housing, and environment. To solve these problems, researchers are working on new transportation systems like urban air mobility (UAM). UAM aircraft should fly safely without burdening the existing air traffic system in the early stage of low-density operation. The airspace should also be managed and operated efficiently. Therefore it is important to make urban air traffic predictable by using corridors and collecting data on low-density operations in the early stage. For this purpose various simulations are needed before operation to create scenarios that estimate potential collisions between UAM aircraft and to evaluate the risks of aircraft spacing, loss of separation (LoS), and near mid air collision (NMAC). This paper focuses on identifying the requirements and considerations for setting separation standards for urban air traffic based on the results of studies.

Concept Design of High Altitude Simulation Test Facility (고공환경모사 시험설비 구축을 위한 개념설계)

  • Kim, Sang-Heon;Kim, Yong-Wook;Lee, Jung-Ho;Yu, Byung-Il;Cho, Sang-Yeon;Oh, Seung-Hyub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2006.11a
    • /
    • pp.75-81
    • /
    • 2006
  • The propulsion system of KSLV-I second stage is engine with high expansion ratio and its starting altitude is high. To verify the performance of engine before the launch in the ground, high altitude test facility to simulate its operating condition is necessary. This material is about the concept design of high altitude simulation test facility for second stage engine. And it will be the basis for the construction of test facility and the test of engine.

  • PDF

해석적 방법을 이용한 Worst Hot 조건에서 질량변화의 여부에 따른 발사시 열해석

  • Kim, Hui-Kyung;Choi, Joon-Min;Hyun, Bum-Seok
    • Aerospace Engineering and Technology
    • /
    • v.3 no.2
    • /
    • pp.42-49
    • /
    • 2004
  • Analytical solutions are developed to predict temperature of a satellite box during launch stage under the assumption of worst hot condition. The considered time period is from fairing jettison to separation of satellite during launch stage. After fairing jettison, a box mounted on outer surface of satellite are exposed to space environments such as direct solar flux, Earth IR, Albedo, and free molecular heating. The thermal governing equation is simplified to 1st order ordinary differential equation such that analytic solutions are acquired after the box is assumed as a single lumped mass. The analytical solutions are also available for mass varying box. Finally, the practical application is performed for the case of STSAT-1 launch scenario.

  • PDF

Development of a Stream Discharge Estimation Program (자연하천 유량산정 프로그램 개발)

  • Lee Sang Jin;Hwang Man Ha;Lee Bae Sung;Ko Ick Hwan
    • Journal of The Korean Society of Agricultural Engineers
    • /
    • v.48 no.1
    • /
    • pp.27-38
    • /
    • 2006
  • In this study, we developed a program to estimate discharge efficiently considering major hydraulic characteristic including water level, river bed, water slope and roughness coefficient in a natural river. Stream discharge was measured at Gongju gauge station located in the down stream of the Daechung Dam during normal and dry seasons from 2003 to 2004. The developed model was compared with the results from the existing rating curve at T/M gage stations, and was used for runoff analyses. Evaluating the developed river discharge estimation program, it was applied during 1983-2004 that base flow separation method and RRFS (Rainfall Runoff Forecasting System) which is based on SSARR (Streamflow Synthesis And Resevoir Regulation). The result presents the stage-discharge curve creator range at the Gong-ju is overestimated by approximately $10-20\%$, especially at the low stage. It is attributed to the hydraulic characteristics at the study. The discharge simulated by the RRFS and base flow separation, which is calibrated using the measurement at the early spring and late fall season during relatively d]v season, shows the least errors. The coefficient of roughness at Gongju station varied with the high and low water level.

The Ablation Effect of Fabric/EPDM Rubber with Manufacturing process (Fabric/EPDM계 고무의 제작 공정에 따른 삭마 특성)

  • Kim, Jin-Yong;Rho, Tae-Ho;Lee, Won-Bok;Cho, Won-Man;Rhee, Young-Woo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2012.05a
    • /
    • pp.92-95
    • /
    • 2012
  • The dual pulse rocket motor is a pressure vessel containing two pulse grains separated by a pulse separation device such as a fragile bulkhead. One of the important things in this systems is case insulation design using the excellent materials in the 1st stage pulse motor. We investigated manufacturing process of fabric/EPDM chamber insulations in order to protect the 1st stage pulse motor case with high intensity gas flow. Simulation motor connected with extension tube having FRP disc was designed to study ablation characteristics of insulation.

  • PDF

Sampling Method for Individual Particle Analysis of Atmospheric Aerosol (개별입자 분석을 위한 대기에어로졸의 시료채취법)

  • Seong-Woo Cheon;Jeong-Ho Park
    • Journal of Environmental Science International
    • /
    • v.33 no.2
    • /
    • pp.113-119
    • /
    • 2024
  • In this study, the most suitable sampling methods for the bimodal mass distribution characteristics and individual particle analysis of atmospheric aerosols were investigated. Samples collected in Quartz, Teflon, and Nuclepore filters were analyzed for individual particles using scanning electron microscopy with an energy-dispersive X-ray spectrometer (SEM/EDS). Then, the pore diameter of the filter and the collection flow rate were determined using the theoretical collection efficiency calculation formula for two-stage separation sample collection of coarse and fine particles. The Nuclepore filter was found to be the most suitable filter for identifying the physical and chemical characteristics of atmospheric aerosols since it was able to separate the sample and count the different sized particles better than either Quartz or Teflon. Nuclepore filters with 8.0 ㎛ and 0.4 ㎛ pores were connected in series and exposed to a flow rate of 16.7 L/min for two-stage separation sampling. The results show that it is possible to separate and collect both coarse and fine particles. We expect that the proposed methodology will be used for future individual particle analysis of atmospheric aerosols and related research.