A new concept using flexible tether-net system to capture space debris is presented in this paper. With a mass point assumption the tether-net system dynamic model is established in orbital frame by applying Lagrange Equations. In order to investigate the net in-plane trajectories during after cast. the non-control R-bar and V-bar captures are simulated with ignoring the out-of-plane ... https://jalyttlers.shop/product-category/room-spray/