• Proceedings of the KIPE Conference
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• 2017.07a
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• pp.457-458
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• 2017

배터리팩의 우주용 어플리케이션은 인공위성 및 발사체로서, 인공위성의 동력원 및 발사체의 순간적인 전력공급을 목적으로 한다. 이 때, 어플리케이션의 요구조건(고전압 및 고용량)에 따라 배터리팩은 리튬계열 셀의 직병렬조합으로 구성된다. 결국, 안정적이고 효율적인 배터리팩의 운용을 위해서는 셀의 고도화가 요구되며, 이의 첫걸음은 셀의 인증(qualification)이라 할 수 있다. 그러므로, 본 논문에서는 인공위성 및 발사체에 사용되는 우주용 셀 인증을 소개하고 이의 비교 분석을 실시한다.

• Aerospace Industry
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• v.30
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• pp.27-31
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• 1995

• Aerospace Industry
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• s.105
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• pp.8-11
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• 2009

• Aerospace Industry
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• v.35
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• pp.16-17
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• 1996

• Current Industrial and Technological Trends in Aerospace
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• v.2 no.2
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• pp.129-136
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• 2004

• Current Industrial and Technological Trends in Aerospace
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• v.1 no.1
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• pp.125-130
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• 2003

• Bulletin of the Korean Space Science Society
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• 2007.10a
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• pp.70.1-70.1
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• 2007

• Bulletin of the Korean Space Science Society
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• 2007.10a
• /
• pp.71.1-71.1
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• 2007

• 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.

• Journal of Aerospace System Engineering
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• v.16 no.4
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• pp.28-34
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• 2022

In 2021, Virgin Orbit converted a 747-400 aircraft into an air launch platform, and successfully launched it twice in February and July. Compared to the existing ground launch, interest in the air launch is increasing due to its great utility, such as its independence from the launch location or weather, cost reducing factor, shorter launch preparation time, and its benefit pursuant to altitude and speed. Additionally, as small satellites have similar performance to mid/large satellites in the past due to the miniaturization and precision of electronic equipment, small satellite launches are expected to dominate in the future. In this paper, institutional certification methods such as domestic, overseas, civilian and military airworthiness certification regulations/procedures are reviewed to ensure flight safety of aerial projectiles using large domestic civil aircraft, and applicable civil and military airworthiness certification technology standards are reviewed and analyzed. Additionally, we will review and suggest effective airworthiness certification application plans that reflect the reality, and present airworthiness certification standards (draft) for aerial launch vehicles, by analyzing applicable airworthiness certification technical standards when remodeling aerial launch vehicles.