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A Temporal Logic for Specification of Dynamic Systems and Its Verification (동적 시스템 명세를 위한 시제논리언어와 그 검증)

  • Cho, Seung-Mo;Kim, Hyung-ho;Cha, Sung-Deok;Bae, Doo-Hwan
    • Journal of KIISE:Software and Applications
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    • v.29 no.7
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    • pp.450-464
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    • 2002
  • Many modern complex systems, including most object-oriented systems, have dynamic characteristics that their components are dynamical]y configured during run-time. However, few analysis techniques are available that consider the dynamic nature of systems explicitly. We propose a specification and analysis method for these dynamic systems. We design a new temporal logic, called HDTL, to specify the properties of dynamically evolving systems, and tune up the tableau method for this logic. HDTL incorporates variables and quantifiers that enable the automatic analysis. Using HDTL and the analysis method, we can specify the correctness requirements of systems and check whether the system actually agree with the requirements or not. An experiment shows that HDTL is suitable for specifying dynamic properties and the analysis technique works well.

Hot-firing Test of Technology Demonstration Model Gas Generator for 75 ton-class Liquid Rocket Engine (75톤급 가스발생기 기술검증시제의 연소시험)

  • Ahn, Kyu-Bok;Seo, Seong-Hyeon;Kim, Mun-Ki;Lim, Byoung-Jik;Kim, Jong-Gyu;Lee, Kwang-Jin;Han, Yeoung-Min;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.225-228
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    • 2009
  • Hot-firing tests were performed on the gas generator which is a technology development/demonstration model for a 75 ton-class liquid rocket engine. A heat-sink type combustion chamber was used for initial performance examination of the injector and mixing head. This paper explains not only preparation works for hot-firing tests but also the acquired results such as pressure, temperature distribution, and pressure fluctuation.

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The Effect of Temperature and Photoinitiator Concentration on Conversion of Photopolymerized Multiethylene Glycol Dimethacrylate by Photo-DSC (Photo-DSC를 사용한 에틸렌글리콜 단위 길이에 따른 다이메타크릴레이트의 광중합 전환률에 미치는 온도와 광개시제 농도의 영향)

  • Do, Hyun-Sung;Kim, Dae-Jun;Kim, Hyun-Joong;Lee, Young-Kyu
    • Journal of Adhesion and Interface
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    • v.4 no.3
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    • pp.14-20
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    • 2003
  • In order to study the radiation curing behavior of poly(ethylene glycol 400) dimethacrylate and ethylene glycol dimethacrylate, we investigated the influence of temperature and photoinitiator concentration by photo-DSC. As the number of ethylene glycol unit, the concentration of photoinitiator, and the reaction temperature increased, the reaction speed of PEG400DMA and EGDMA increased. Although the reaction speed of PEG400DMA was lower than EGDMA, the overall conversion of PEG400DMA was high.

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Combustion Characteristics of Technology Demonstration Model for Staged Combustion Cycle Engine (다단연소사이클 엔진 시스템 기술검증시제 연소성능 평가)

  • Im, Ji-Hyuk;Woo, Seongphil;Jeon, Junsu;Lee, Jungho;Lee, Kwang-Jin;Han, Yeoung-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.108-111
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    • 2017
  • High performance upper stage engine is necessary for space launch vehicles of geostationary orbit, and staged combustion cycle engine is suitable due to high specific impulse. Technology demonstration model for 9 tonf class staged combustion cycle engine, which is consisted of turbopump, preburner, combustion chamber and supply system, was assembled, and hot-firing test was conducted for three seconds in Upper-stage Engine Test Facility of Naro Space Center. Ignition, combustion and shut down of engine system was performed normally, and its performance parameters were evaluated.

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Design and Fabrication of Technology Demonstration Model of 75 tonf Regenerative Cooling Thrust Chamber (75톤급 재생냉각 연소기 기술검증용 시제 설계 및 제작)

  • Kim, Jong-Gyu;Ahn, Kyu-Bok;Lim, Byoung-Jik;Kim, Mun-Ki;Kang, Dong-Hyuk;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.31-34
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    • 2011
  • Design and fabrication of Technology Demonstration Model(TDM) of 75 tonf regenerative cooling thrust chamber were described. It has design chamber pressure of 60 bar, propellant mass flow rate of 243.6 kg/s, and nozzle expansion ratio of 12. It has a single welded structure of the mixing head and the chamber. Design and fabrication technologies established through this TDM can be used to development of flight model.

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Tempussystem und Tempusgebrauch im Deutschen (독일어의 시제체계와 쓰임에 관하여)

  • Park Hyun-Sun
    • Koreanishche Zeitschrift fur Deutsche Sprachwissenschaft
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    • v.6
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    • pp.241-261
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    • 2002
  • In der Grammatik $f\"{u}r$ die Lernenden werden die deutschen Tempora nach dem lateinischen Vorbild dargestellt: $Pr\"{a}sens,\;Pr\"{a}teritum$, Perfekt, Plusquamperfekt, Futur I und Futur II. Und diese sechs Tempora werden in die drei Zeitstufen kIassifiziert: Gegenwart, Vergangenheit und Zukunft. Aber die Zeitformen $k\"{o}nnen$ nicht in direkter und geradliniger Weise auf bestimmte objektive Zeiten beziehen. Das $Verh\"{a}ltnis$ zwischen Zeitinhalt und Zeitform ist verwickelter und komplexer. Man denkt nach, wie viele Tempora es in der deutschen Sprache gibt und warum die Tempora Funktionen, die nicht nur Zeitinhalt, sondern auch andere Inhalte(z.B. modale) $ausdr\"{u}ken$, haben. Urn die Probleme zu $erl\"{a}utern$, sollen wir die deutschen Tempora von der lateinischen Tempuskategorie abtrennen und ein geeignetes Tempussystem $f\"{u}r$ die deutsche Sprache suchen. Dazu $m\"{u}ssen$ wir beobachten, Wie die deutschen Tempora konstruiert wurden. Im Lateinischen handelt es sich bei allen sechs Tempora um Verbformen, um bestimmte ($n\"{a}mlich$ die indikativischen) Formen des finiten Verbs. Im Deutschen aber finden wir unter den Tempora nur zwei richtige Verbformen $(Pr\"{a}sens\;und\;Pr\"{a}teriturn),\;die\;\"{u}brigen$ Tempora sind verbale Komplexe, drei zweiwortige (Perfekt, Plusquamperfekt, Futur I) und ein dreiwortiger (Futur II). Und das deutsche Tempussystem besteht aus den zwei Polen: Vergangenes und Nicht-Vergangenes oder $Temporalit\"{a}t\;und\;Atemporalit\"{a}t$. Die Tempusform $Pr\"{a}teritum\;geh\"{o}rt\;zu\;Temporalit\"{a}t$ und die Tempusform $Pr\"{a}sens\;zu\;Atemporalit\"{a}t$. Das $Pr\"{a}sens\;und\;das\;Pr\"{a}teritum$ sind die Grundtempora im Deutschen und die $\"{u}brigen$ Tempora sind die durch den Aspekt erweiterten und die zusammengesetzten Tempora. Sie haben deswegen die inneren Merkmale Aspekt und Modale $au{\ss}er$ Zeitbezug. Wir $k\"{o}nnen$ diese inneren Merkmale im Tempusgebrauch feststellen. Als Funktionen der Tempora der deutschen Sprache im Tempusgebrauch sind zu registrieren: Bezeichnung zeitlicher Gegebenheit, modale Implikationen, Aspektangaben und semantische Akzentuierungen. Und noch eins: Die Funktion des neutralen Referieren des Inhaltes durch das atemporale $Pr\"{a}sens$. Das $Pr\"{a}sens$ wird durch diese Referentfunktion zu dem Haupttempus auch in der geschriebenen Sprache. Trotzdem nennt man das $Pr\"{a}teritum$ in der geschriebenen Sprache das Haupttempus. Ist das $Pr\"{a}teritum$ dann in der Tat in der geschriebenen Sprache das Haupttempus? Genau genommen ist das $Pr\"{a}sens$ offenbar ein Haupttempus. Es wird nicht nur in der gesprochenen Sprache, sowohl auch in den geschriebenen nichtbelletristischen Texten $haupts\"{a}chlich$ benutzt. Aber nur die belletristischen Texte werden durch das $Pr\"{a}teritum$ beherrscht. Der Gebrauch des $Pr\"{a}teritums$ als Haupttempus $beschr\"{a}nkt$ sich nur auf die Belletristik. Wir glauben, die Untersuchung $\"{u}ber$ den Tempusgebrauch und die Tempusfunktion in den verschiedenen Textsorten sei besonders dem Nichtmuttersprachler wichtig, weil die Textsorten beim Tempusgebrauch eine Wahl des Tempus beeinflussen.

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UV Curing and Peeling Characteristics of Acrylic Coating Ink with Various Amounts of Photoinitiator, Oligomer and Talc (광개시제, 올리고머 그리고 Talc 함량에 따른 아크릴계 코팅제의 UV경화 및 박리특성)

  • Yang, Jee-Woo;Seo, Ah Young;Lee, Chul Woo
    • Applied Chemistry for Engineering
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    • v.24 no.5
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    • pp.499-506
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    • 2013
  • As the usuage of tempered glass for touch panel increased rapidly with the development of industry, the amount of UV curable coating solution used to protect glass surfaces during a tempered glass manufacturing process increased as well. The UV curable coating has advantages compared to thermal curing such as shortened curing time and non-solvent. Appropriated polymer and monomer were used as an acid polymer to grant an alkali peeling ability. The monomers were 2-hydroxyl methylacrylate, 1,6-hexanediol diacrylate and dipentaerythritol hexaacrylate which have acryl groups of 1, 2, and 6, respectively. The combination of three different types of photoinhibitors were used and bisphenol A epoxy diacrylate was used as an oligomer. In this study, experiments were carried out by controlling the amount of photoinitiator, oligomer, and additive while maintaining the constant content of the acid polymer and the acrylic monomer. The changes in physical properties according to the additive content were investigated. It was found that the combination of photoinitiators was necessary to achieve the hardness above 4H and it was possible to control the delamination type of the coating film from a sheet to pieces by the addition of TPO as an initiator. The increase in oligomer contents increased the hardness and adhesiveness alongside dissection time. Talc content of 20 wt% showed the best results.

Effect of the difference in spectral outputs of the single and dual-peak LEDs on the microhardness and the color stability of resin composites (Single-peak LED와 dual-peak LED의 출력 파장 차이가 복합 레진 미세 경도와 색 안정성에 미치는 영향)

  • Park, Hye-Jung;Son, Sung-Ae;Hur, Bock;Kim, Hyeon-Cheol;Kwon, Yong-Hoon;Park, Jeong-Kil
    • Restorative Dentistry and Endodontics
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    • v.36 no.2
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    • pp.108-113
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    • 2011
  • Objectives: To determine the effect of the spectral output of single and dual-peak light emitting diode (LED) curing lights on the microhardness and color stability of commercial resin composites formulated with camphorquinone and alternative photoinitiators in combination. Materials and Methods: Three light-polymerized resin composites (Z100 (3M ESPE), Tetric Ceram (Ivoclar Vivadent) and Aelite LS Posterior (Bisco)) with different photoinitiator systems were used. The resin composites were packed into a Teflon mold (8 mm diameter and 2 mm thickness) on a cover glass. After packing the composites, they were light cured with single-peak and dual-peak LEDs. The Knoop microhardness (KHN) and color difference (${\Delta}E$) for 30 days were measured. The data was analyzed statistically using a student's t-test (p < 0.05). Results: All resin composites showed improved microhardness when a third-generation dual-peak LED light was used. The color stability was also higher for all resin composites with dual-peak LEDs. However, there was a significant difference only for Aelite LS Posterior. Conclusions: The dual-peak LEDs have a beneficial effect on the microhardness and color stability of resin composites formulated with a combination of camphorquinone and alternative photoinitiators.

Launch Environment Test for Scale magNetospheric and Ionospheric Plasma Experiment (SNIPE) Engineering Qualification Model (초소형위성 SNIPE(Scale Magnetospheric and Ionospheric Plasma Experiment) 시제인증모델의 발사환경시험 및 분석)

  • Kim, Min-Ki;Kim, Hae-Dong;Choi, Won-Sub;Kim, Jin-Hyung;Kim, KiDuck;Kim, Ji-Seok;Cho, Dong-Hyun
    • Journal of Space Technology and Applications
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    • v.1 no.3
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    • pp.319-336
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    • 2021
  • This paper discusses the results of launch environment tests for the engineering qualification model (EQM) of nanosatellite Scale magNetospheric and Ionospheric Plasma Experiment (SNIPE) for scientific missions and lessons learned for the design of nanosatellites. SNIPE is a group of four formation-flying 6U nanosatellites with a range of payloads for missions including space weather measurement. We developed the EQM to verify the preliminary design prior to fabricating the flight model. Launch environment test of EQM was conducted for the first time in 2019, and all failures were corrected and verified at the second test conducted in 2021. A notable point of the two tests is that the nanosatellite deployer used in the first test is different from that of the second test. The second deployer has the capability to fix the internal satellite whereas the first deployer just contains and deploys the satellite. Thus actual mechanical loads the satellite receives is reduced for the second test compared to the first test. This work compares the mechanical responses of two tests and proposes general guidelines for structural design of nanosatellites.