¿¬±¸¼º°ú HOME > ÁÖ¿ä»ç¾÷¼º°ú > ¿¬±¸¼º°ú > ³í¹®
ÃâÀ帶»çÁöÃâÀå¾È¸¶
 
Potential trajectory design for a lunar CubeSat impactor deployed from a HEPO using only a small separation delta-V
°ü¸®ÀÚ 1,798

Potential trajectory design for a lunar CubeSat impactor deployed from a HEPO using only a small separation delta-V


Song, Young-Joo; Lee, Donghun; Jin, Ho; Kim, Bang-Yeop

Advances in Space Research, Volume 59, Issue 2, p. 619-630. (AdSpR Homepage)