포고핀을 활용한 극초소형 위성용 태양전지판 분리장치의 기능검증

김수현 전영현 김홍래 오현웅 2018년

논문상세정보

인용/피인용

한국의 큐브위성 개발 현황 분석
한상혁 [2017]
https://www.planet.com
http://www.pumpkinspace.com/
http://www.hanbittni.com/
Verification of MEMS Fabrication Process for the Application of MEMS Solid Propellant Thruster Arrays in Space through Launch and On-orbit Environment Tests
H. U. Oh [2017]
Tokyo Tech Cubesat: CUTE-I-Design & Development of Flight Model and Future Plan
K. Nakaya [2003]
Performance Verification of Solar Panel Deployment Mechanism for Cube-Sat Applications Using Pogo-pin
S. H. Kim [2018]
Performance Evaluation of Hinge Driving Separation Nut-type Holding and Releasing Mechanism Triggered by Nichrome Burn Wire
이명재 [2015]
Nanosatellites for Earth Environmental Monitoring: The MicroMAS Project
W. Blackwell [2012]
Integrated Design of Solar Panels Deployment Mechanism for a Three Unit Cubesat
B. Hamza [2012]
Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels
T. Y. Park [2018]
Cubesats: Cost-effective Science and Technology Platforms for Emerging and Developing Nations
K. Woellert [2011]