TY - GEN
T1 - Development of net-ejector for active debris removal using spacenet
AU - Kim, Sejun
AU - Song, Dahan
AU - Kim, Hyejin
AU - Cho, Haeseong
N1 - Publisher Copyright:
© 2024 15th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2024. All rights reserved.
PY - 2024
Y1 - 2024
N2 - In this study, a net-ejector for net-based active debris removal is developed. The capture method using a net involves the ejection of the net as a projectile attached to the end of the net. Therefore, for successful mission, the design of an appropriate net-shooter for net ejection is essential. Accordingly, a net-shooter for net-based active debris removal mission is designed. The net-shooter utilizes an ejection mechanism based on the elastic restoration force of a compressed spring and a hold and release mechanism using a DC motor and holding balls. Additionally, a spring is designed, and the verification of spring design is conducted through a dynamic ejection simulation. Through the spring specifications, a spring-based non-explosive net-shooter is designed. The robustness of the net-shooter for spring elastic restoration force and the random vibration analysis considering a launch environment is evaluated. Moreover, a scaled model of the spring-based non-explosive net-shooter is designed for ground test. This scaled net-shooter is designed through the same process as the full-scale net-shooter, and its fabrication is carried out through the 3D printing. Subsequently, The demonstration is conducted to evaluate the performance of the mechanism. As a result, it is confirmed that both the projecitle and the net are successfully ejected from the designed spring-based non-explosive net-shooter.
AB - In this study, a net-ejector for net-based active debris removal is developed. The capture method using a net involves the ejection of the net as a projectile attached to the end of the net. Therefore, for successful mission, the design of an appropriate net-shooter for net ejection is essential. Accordingly, a net-shooter for net-based active debris removal mission is designed. The net-shooter utilizes an ejection mechanism based on the elastic restoration force of a compressed spring and a hold and release mechanism using a DC motor and holding balls. Additionally, a spring is designed, and the verification of spring design is conducted through a dynamic ejection simulation. Through the spring specifications, a spring-based non-explosive net-shooter is designed. The robustness of the net-shooter for spring elastic restoration force and the random vibration analysis considering a launch environment is evaluated. Moreover, a scaled model of the spring-based non-explosive net-shooter is designed for ground test. This scaled net-shooter is designed through the same process as the full-scale net-shooter, and its fabrication is carried out through the 3D printing. Subsequently, The demonstration is conducted to evaluate the performance of the mechanism. As a result, it is confirmed that both the projecitle and the net are successfully ejected from the designed spring-based non-explosive net-shooter.
UR - https://www.scopus.com/pages/publications/105014916664
M3 - Conference paper
AN - SCOPUS:105014916664
T3 - 15th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2024
SP - 164
EP - 173
BT - 15th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2024
T2 - 15th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2024
Y2 - 28 October 2024 through 30 October 2024
ER -