• 제목/요약/키워드: microgravity environment

검색결과 30건 처리시간 0.024초

Experiment Investigation on Fluid Transportation Performance of Propellant Acquisition Vanes in Microgravity Environment

  • Zhuang, Baotang;Li, Yong;Luo, Xianwu;Pan, Halin;Ji, Jingjing
    • International Journal of Fluid Machinery and Systems
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    • 제7권1호
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    • pp.1-6
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    • 2014
  • The propellant acquisition vane (PAV) is a key part of a vane type surface tension propellant management device (PMD), which can manage the propellant effectively. In the present paper, the fluid transportation behaviors for five PAVs with different sections were investigated by using microgravity drop tower test. Further, numerical simulation for the propellant flow in a PMD under microgravity condition was also carried out based on VOF model, and showed the similar flow pattern for PAVs to the experiment. It is noted that the section geometry of PAVs is one of the main factors affecting the fluid transportation behavior of PMD. PAVs with bottom length ratio of 5/6 and 1/2 have larger propellant transportation velocity. Based on the experiments, there were two stages during the process of propellant transportation under microgravity environment: liquid relocation and steady transportation stage. It is also recognized that there is a linear correlation between liquid transportation velocity and relative time's square root. Those results can not only provide a guideline for optimization of new vane type PMDs, but also are helpful for fluid control applications in space environment.

미소중력 환경내의 벽면 근방 확산 화염 특성에 관한 수치 해석 (Numerical Simulation on Characteristics of Laminar Diffusion Flame Placed Near Wall in Microgravity Environment)

  • 최재혁;후지타 오사무
    • Journal of Advanced Marine Engineering and Technology
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    • 제30권1호
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    • pp.140-149
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    • 2006
  • Characteristics of a laminar diffusion flame placed near wall in microgravity have been numerically analyzed in a two-dimension. The fuel for the flame is $C_2H_4$. The flame is initiated by imposing a high temperature ignition source. The flow field, temperature field, and flame shape in microgravity diffusion flame are detailed. Especially, effects of surrounding air velocity and fuel injection velocity on the microgravity diffusion flame have been discussed accounting for standoff distance. And, the effect of curvature rate has been also studied. The results showed that velocities in a diffusion flame were overshoot because of volumetric expansion and distribution of temperature showed regularity by free-buoyancy This means that the diffusion flame in microgravity is very stable, while the flame in normal gravity is not regular and unstable due to buoyancy. Standoff distance decreases with increase in surrounding air velocity and with decrease in fuel injection velocity. With increasing curvature rate, the position of reaction rate moves away the wall.

Effects of Microgravity on Vestibular Development and Function in Rats: Genetics and Environment

  • Ronca, April-E.;Fritzsch, Bernd;Alberts, Jeffrey-R.;Bruce, Laura-L.
    • Animal cells and systems
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    • 제4권3호
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    • pp.215-221
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    • 2000
  • Our anatomical and behavioral studies of embryonic rats that developed in microgravity suggest that the vestibular sensory system, like the visual system, has genetically mediated precesses of development that establish crude connections between the periphery and the brain. Environmental stimuli also regulate connection formation including terminal branch formation and fine-tuning of synaptic contacts. Axons of vestibular sensory neurons from grabistatic as well as linear acceleration receptors reach their targets in both microgravity and norm81 gravity, suggesting that this is a genetically regulated component of development. However, microgravity exposure delays the development of terminal branches and synapses in gravistatic but not linear acceleration-sensitive neurons and also produces behavioral changes. These latter changes reflect environmentally controlled processes of development.

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Conceptual Design and Demonstration of Space Scale for Measuring Mass in Microgravity Environment

  • Kim, Youn-Kyu;Lee, Joo-Hee;Choi, Gi-Hyuk;Choi, Ik-Hyeon
    • Journal of Astronomy and Space Sciences
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    • 제32권4호
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    • pp.419-425
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    • 2015
  • In this study, a new idea for developing a space scale for measuring mass in a microgravity environment was proposed by using the inertial force properties of an object to measure its mass. The space scale detected the momentum change of the specimen and reference masses by using a load-cell sensor as the force transducer based on Newton's laws of motion. In addition, the space scale calculated the specimen mass by comparing the inertial forces of the specimen and reference masses in the same acceleration field. By using this concept, a space scale with a capacity of 3 kg based on the law of momentum conservation was implemented and demonstrated under microgravity conditions onboard International Space Station (ISS) with an accuracy of ${\pm}1g$. By the performance analysis on the space scale, it was verified that an instrument with a compact size could be implemented and be quickly measured with a reasonable accuracy under microgravity conditions.

공유 지상국을 활용하여 획득한 마이크로중력 과학임무 큐브위성의 운영 결과와 교훈 (Results and Lessons Learned from the Operation of a Cubesat for the Microgravity Science Mission with Shared Ground Stations)

  • 이명규;박설현
    • 우주기술과 응용
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    • 제4권2호
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    • pp.137-152
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    • 2024
  • 현재 마이크로중력 환경을 활용한 과학실험은 초 단위 정도의 짧은 시간 동안 실험이 수행 가능한 낙하 탑부터 시간제한이 없는 우주정거장 등 여러 분야에서 수행되고 있다. 하지만 과학 실험에 필요한 긴 시간이 확보된 마이크로중력 환경을 구현하기 위해서는 적지 않은 개발비용과 시간이 소모된다. 따라서 고비용이 수반되는 마이크로중력 환경 실험을 큐브위성에서 수행한다면 저비용 고효율의 이점으로 과학 실험의 다양성과 시간의 제약에서 자유도가 더욱 높아질 것으로 판단된다. 이러한 특장점을 살린 KMSL(Korea Microgravity Science Laboratory) 큐브위성은 마이크로중력 환경에서의 과학 임무를 수행하였던 위성이다. KMSL 위성은 2021년 3월 22일 카자흐스탄 바이코누르 발사기지에서 Soyuz2.1a 발사체에 의해 발사되었고, 약 2개월간 정상적으로 임무를 수행하였다. 본 논문에서는 KMSL 위성의 운영 경험과 발생한 문제에 대한 분석을 바탕으로 마이크로중력 환경에서의 과학 임무를 성공적으로 수행하기 위한 해결책과 교훈을 제시하고자 한다.

Effects of Microgravity on Human Physiology

  • Nguyen, Nguyen;Kim, Gyutae;Kim, Kyu-Sung
    • 항공우주의학회지
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    • 제30권1호
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    • pp.25-29
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    • 2020
  • Space exploration is one of the dreams of humankind. However, the intriguing environment was a challenge for the human body, where we must counter with many extreme conditions such as thermal support, radiation, microgravity. Life, as well as the human body, developed and evolved in the continuous presence of gravity, especially when living creatures transfer from the ocean to the land. Once this gravitational force doesn't impact on the body, the drastic changes occur. Some of these changes were observed immediately, while others progress only slowly. Since the first orbital flight was performed, several hazards for the organs of the human body were identified [1]. These changes in human physiology can reverse when astronauts return to Earth. This article will review the published findings of the effects of microgravity exposure on the human body.

미소중력환경을 이용한 벽면근방 확산화염내 매연부착거동의 원위치 관찰 (In-situ Observation of Soot Deposition Behavior in a Diffusion Flame along Solid Wall by using Microgravity Environment)

  • 최재혁;후지타 오사무
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권8호
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    • pp.907-914
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    • 2005
  • Experiments at the Japan Microgravity Center (JAMIC) have investigated the interaction between diffusion flames and solid surfaces Placed neat flames The fuel for the flames was $C_{2} H_{4}$ The surrounding oxygen concentration was 35$\%$ with surrounding air temperatures of $T_{a}$ : 300K. Especially, the effect of wall temperature on soot deposition from a diffusion flame Placed near the wall has been studied by utilizing microgravity environment, which can attain very stable flame along the wall. Cylindrical burner with fuel injection was adopted to obtain two dimensional soot distributions by laser extinction method. In the experiment two different wall temperatures. $T_{w}$=300, 800 K, were selected as test conditions The results showed that the soot distribution between flame and burner wall was strong1y affected by the wall temperature and soot deposition increases with decrease in wall temperature. The comparison among the values lot two different wall temperatures suggests that the change in thermophoretic effect is the most dominant factor to give the change in soot deposition characteristics.

미소중력환경에서의 고체벽면근방 층류확산염내 매연입자의 열영동 부착 (Thermophoretic deposition of soot particles in laminar diffusion flame along a solid wall in microgravity)

  • 최재혁;후지타오사무;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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    • pp.19-24
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    • 2007
  • The deposition behavior of soot particles in a diffusion flame along a solid wall was examined experimentally by getting rid of the effect of natural convection utilizing microgravity environment. The microgravity environment was realized by using a drop tower facility. The fuel for the flame was an ethylene ($C_2H_4$) and the surrounding oxygen concentration 35% with the surrounding air velocity of $V_a$=2.5, 5, and 10 cm/s. Laser extinction method was adopted to measure the soot volume fraction distribution between the flame and burner wall. The results show that observation of soot deposition in normal flame was difficult from buoyancy and the relative position of flame and solid surface changes with time. The soot particle distribution region moves closer to the surface of the wall as the surrounding air velocity is increased. And the experiments determined the trace of the maximum soot concentration line. It was found that the distance between soot line and flame line is around 5 mm. That is, the soot particle near the flame zone tends to move away from flame zone because of thermophoretic force and to concentrate at a certain narrow area inside of the flame, finally, to adhere the solid wall.

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미소중력환경하에서의 확산화염내 매연입자의 벽면부착 관찰 (Soot Deposition Process in a Diffusion Flame to the Wall under Microgravity)

  • 최재혁;후지타오사무;윤석훈
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2005년도 전기학술대회논문집
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    • pp.87-92
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    • 2005
  • Experiments at the Japan Microgravity Center(JAMIC) have investigated the interaction between diffusion flames and solid surfaces placed near flames. The fuel for the flames was $C_2H_4$. The surrounding oxygen concentration was 35% with temperatures of $T_a$=300. Especially, the effect of wall temperature on soot deposition from a diffusion flame placed near the wall has been studied by utilizing microgravity environment, which can attain very stable flame along the wall. Cylindrical burner with fuel injection was adopted to obtain two dimensional soot distributions by laser extinction method. In the experiment two different wall temperatures, $T_w$=300,800K, were selected as test conditions. The results showed that the soot distribution between flame and burner wall was strongly affected by the wall temperature and soot deposition increases with decrease in wall temperature. The comparison among the values for two different wall temperatures suggested that the change in thermophoretic effect is the most dominant factor to give the change in soot deposition characteristics.

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Effects of Solutally Dominant Convection on Physical Vapor Transport for a Mixture of Hg2Br2 and Br2 under Microgravity Environments

  • Kim, Geug-Tae;Kwon, Moo Hyun
    • Korean Chemical Engineering Research
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    • 제52권1호
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    • pp.75-80
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    • 2014
  • The convective flow structures in the vapor phase on earth are shown to be single unicellular, indicating the solutally dominant convection is important. These findings reflect that the total molar fluxes show asymmetrical patterns in a viewpoint of interfacial distributions. With decreasing the gravitational level form $1g_0$ down to $1.0{\times}10^{-4}g_0$, the total molar fluxes decay first order exponentially. It is also found that the total molar fluxes decay first order exponentially with increasing the partial pressure of component B, PB (Torr) form 5 Torr up to 400 Torr. Under microgravity environments less than $1g_0$, a diffusive-convection mode is dominant and, results in much uniformity in front of the crystal regions in comparisons with a normal gravity acceleration of $1g_0$.