• International Journal of Aeronautical and Space Sciences
• /
• 제17권4호
• /
• pp.526-534
• /
• 2016

A MEMS solid propellant thruster array shall be operated within an allowable range of operating temperatures to avoid ignition failure by incomplete combustion due to a time delay in ignition. The structural safety of the MEMS thruster array under severe on-orbit thermal conditions can also be guaranteed by a suitable thermal control. In this study, we propose a thermal control strategy to perform on-orbit verification of a MEMS thruster module, which is expected to be the primary payload of the STEP Cube Lab mission. The strategy involves, the use of micro-igniters as heaters and temperature sensors for active thermal control because an additional heater cannot be implemented in the current design. In addition, we made efforts to reduce the launch loads transmitted to the MEMS thruster module at the system level structural design. The effectiveness of the proposed thermo-mechanical design strategy has been demonstrated by numerical analysis.

• 우주기술과 응용
• /
• 제3권3호
• /
• pp.213-228
• /
• 2023

무인 탐사로버는 지구가 아닌 타 행성체에서 인간을 대신해 광물자원의 조사와 채굴 또는 여러 가지 과학 미션을 진행하는 도구로써 사용되고 있다. 최근에는 미국이 아닌 일본, 인도, 중국 등 여러 국가에서 우주개발을 위한 무인 행성 탐사로버의 개발을 시도하거나 실제 타 행성체에서 주행에 성공하는 사례가 생기며 우주로 향한 개발열풍이 가속화되고 있다. 하지만 여전히 행성을 탐사하기 위한 무인 로버의 개발과 운용은 천문학적인 비용이 수반되는 위험도가 높은 계획이며, 국가나 정부차원의 주도가 아닌 대학 또는 기업에서 독자적으로 개발을 시도하기에는 현실적인 제약이 크게 따른다. 본 논문에서는 기존의 큐브위성의 개념과 정의를 계승한 큐브로버와 (초)소형 로버의 최근 개발동향을 소개하고 큐브로버 개발의 필요성과 함께 현재 진행되고 있는 행성탐사 사례를 들어 큐브로버의 가능성과 기대사항을 소개하고자 한다.

• 한국기계가공학회지
• /
• 제13권5호
• /
• pp.64-69
• /
• 2014

This article presents machining experiments to assess the relationship between the profile accuracy and the workpiece hardness using a natural diamond tool on an ultra-precision diamond turning machine. The study is intended to secure a corner cube prism pattern for reflective film capable of high-quality outcomes. The optical performance levels and edge images of corner cubes having various hardness levels of the copper-coated layer on a carbon steel plate are analyzed. The hardness of the workpiece has a considerable effect on the profile accuracy. The higher the hardness of the workpiece, the better the profile accuracy and the worse the edge wear of the diamond tool.

• 항공우주시스템공학회지
• /
• 제11권5호
• /
• pp.65-75
• /
• 2017

본 연구에서는 3U 큐브위성의 표준 플랫폼을 개발하였으며, 개발된 표준 플랫폼을 3U 큐브위성인 한누리 5호에 적용함으로써 기능 및 성능을 검증하였다. 표준 플랫폼의 설계를 위해 기존 큐브위성 및 최신기술을 조사하여 3U 큐브위성 플랫폼 규격을 선정하였으며, 범용적으로 사용이 가능하도록 설계하였다. 표준 플랫폼은 1.5U 크기로 설계 및 제작되었고, 모듈러 개념으로 개발되어 사용자의 요구임무에 맞게 탑재체와 자세제어 구동기 등을 추가 및 확장시킬 수 있다. 또한 전력계의 경우 태양전지판, 배터리 및 전개 메커니즘을 사용자가 직접 구성하도록 설계하였다. 기계시스템 설계에서는 초소형 부품 및 서브시스템 기능/성능을 초소형 PCB에 집적 및 소형화하도록 하고, 다양한 탑재체를 수용할 수 있도록 플랫폼의 공간 활용률을 극대화하였다. 3U 큐브위성 개발 시, 위성 플랫폼은 개발된 표준 플랫폼을 채택하여 추가적인 기능 검증 등을 줄여 전체 위성개발에 대한 비용 및 일정을 단축시킬 수 있다.

• 천문학회보
• /
• 제46권1호
• /
• pp.58.4-59
• /
• 2021

This presentation introduces Korea's SNIPE (Small scale magNespheric and Ionospheric Plasma Experiment) mission, formation flying CubeSat constellation. Observing particles and waves on a single satellite suffers from inherent space-time ambiguity. To observe spatial and temporal variations of the micro-scale plasma structures on the topside ionosphere, four 6U CubeSats (~ 10 kg) will be launched into a polar orbit of the altitude of ~500 km in 2021. The distances of each satellite will be controlled from 10 km to more than 100 km by formation flying algorithm. The SNIPE mission is equipped with identical scientific instruments, solid-state telescope, magnetometer, and Langmuir probe. All the payloads have a high temporal resolution (sampling rates of about 10 Hz). Iridium modules provide an opportunity to upload changes in operational modes when geomagnetic storms occur. SNIPE's observations of the dimensions, occurrence rates, amplitudes, and spatiotemporal evolution of polar cap patches, field-aligned currents (FAC), radiation belt microbursts, and equatorial and mid-latitude plasma blobs and bubbles will determine their significance to the solar wind-magnetosphere-ionosphere interaction and quantify their impact on space weather.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2008년도 제39회 하계학술대회
• /
• pp.1454-1455
• /
• 2008

This paper present a piezoelectric actuated mirror with PZT cantilevers, torsional bars and hinges for Micro-CCR (corner cube retroreflector). The actuated mirror with low voltage and large tilting angle is designed and simulated by using FEM (Finite Element Method) simulator (CoventorWare). The tilting angle of actuated mirror is 2.93$^{\circ}$ at low voltage of 5V.

• 한국추진공학회지
• /
• 제5권3호
• /
• pp.100-107
• /
• 2001

Miro propulsion device is a literally very small propulsion system The reason why such a small propulsion system is required is that micro satellites are considered as substitutions for conventional satellites to reduce cost; the fabrication of micro satellites enables us to produce mass production Microrockets have relatively high values of thrust/weight ratio due to the cube law; weight is proportional to volume and thrust is proportional to area. Accordingly, downsizing makes the ratio of thrust/weight ratio high However, conventionally ignorable facts are not negligible any more in small scale systems. for chemical micro rockets, downsizing causes lots of heat loss as surface to volume ratio increases, which results in the destruction of radical ions. For thrusters using plasma, the generation of strong magnetic field for plasma is very difficult. Also, in the aspect of flow dynamics, the effects of drag and viscosity are important parameters in low Re flows. When these problems are solved, micro propulsion systems can be commercialized and result in spin-off effects in many fields.

• Progress in Superconductivity
• /
• 제6권1호
• /
• pp.64-68
• /
• 2004

We fabricated cube-textured Ni and Ni-W alloy substrates for coated conductors and characterized the effects of W addition on microstructure, mechanical strength, and magnetic properties of the substrate. Pure Ni and Ni-(2, 3, 5at.%)W alloys were prepared by plasma arc melting, heavily cold rolled and then annealed at various temperatures of $600-1300^{\circ}C$. The texture was evaluated by pole-figure and orientation distribution function (ODF) analysis. Mechanical properties were investigated by micro Vickers hardness and tension test. Ferromagnetism of the substrate was measured by physical property measurement system (PPMS). It was observed that Ni-W substrates had sharp cube texture, and the full-width at half-maximums (FWHMs) of in-plane texture was $^{\circ}$-5.57$4.42^{\circ}$, which is better than that of pure Ni substrate. In addition cube texture of Ni-W substrates was retained at higher temperature up to $1300^{\circ}C$. Microstructural observation showed that the Ni-W substrates had fine grain size and higher mechanical properties than the pure Ni substrate. These improvements are probably due to strengthening mechanisms such as solid solution hardening and/or grain size strengthening. PPMS analysis showed that addition of W effectively reduced saturation magnetization in applied magnetic field and Curie temperature.

• Journal of Electrical Engineering and Technology
• /
• 제5권2호
• /
• pp.337-341
• /
• 2010

In this paper, an extremely low voltage operated micro corner cube retroreflector (CCR) was fabricated for free-space optical communication applications by using bulk silicon micromachining technologies. The CCR was comprised of an orthogonal vertical mirror and a horizontal actuated mirror. For low voltage operation, the horizontal actuated mirror was designed with two PZT cantilever actuators, torsional bars, hinges, and a mirror plate with a size of $400{\mu}m{\times}400{\mu}m$. In particular, the torsional bars and hinges were carefully simulated and designed to secure the flatness of the mirror plate by using a finite element method (FEM) simulator. The measured tilting angle was approximately $2^{\circ}$ at the applied voltage of 5 V. An orthogonal vertical mirror with an extremely smooth surface texture was fabricated using KOH wet etching and a double-SOI (silicon-on-insulator) wafer with a (110) silicon wafer. The fabricated orthogonal vertical mirror was comprised of four pairs of two mutually orthogonal flat mirrors with $400{\mu}m4 (length) $\times400{\mu}m$ (height) $\times30{\mu}m$ (thickness). The cross angles and surface roughness of the orthogonal vertical mirror were orthogonal, almost $90^{\circ}$ and 3.523 nm rms, respectively. The proposed CCR was completed by combining the orthogonal vertical and horizontal actuated mirrors. Data transmission and modulation at a frequency of 10 Hz was successfully demonstrated using the fabricated CCR at a distance of approximately 50 cm.

• 한국정밀공학회지
• /
• 제27권8호
• /
• pp.91-97
• /
• 2010

Micro-abrasive Jet Machining is one of the new technology which enables micro-scale machining on the surface of high brittle materials. In this technology it is very important to fabricate a mask that prevents excessive abrasives not to machine un-intend surface. Our previous work introduced the micro-stereolithography technology for the mask fabrication. And is good to not only planar material but also for non-planar materials. But the technology requires a 3 dimensional mask CAD model which is perfectly matched with the surface topology of parent material as an input. Therefore there is strong need to develop an automated modeling technology which produce adequate 3D mask CAD model in fast and simple way. This paper introduces a fast and simple mask modeling algorithm which represents geometry of models in voxel. Input of the modeling system is 2D pattern image, 3D CAD model of parent material and machining parameters for Micro-abrasive Jet Machining. And the output is CAD model of 3D mask which reflects machining parameters and geometry of the parent material. Finally the suggested algorithm is implemented as software and verified by some test cases.