viewimage.php?id=3abcc2&no=24b0d769e1d32ca73cee86fa11d0283191de25edc716dfae8790c63e5c69dc5d515c34173a20cc10152e26ecf3d09dc925cacf20469300999f9c6c65c65db96ed15f28a0edfb23d3b9835c96

viewimage.php?id=3abcc2&no=24b0d769e1d32ca73cee86fa11d0283191de25edc716dfae8790c63e5c69dc5d515c34173a20cc10152e26ecf3d09dc925cac72047c250cacbc86c65c151b82bf5d4f1443620bbb656476a182896447f3ef6709156a4f587a4562062a5880e37c6fe5ae846

viewimage.php?id=3abcc2&no=24b0d769e1d32ca73cee86fa11d0283191de25edc716dfae8790c63e5c69dc5d515c34173a20cc10152e26ecf3d09dc925ca9c2149c10093cfcf6c06b744b86aff98d3b415d6e41a911a8a


SSME: 1,860kN, 추중비 73.1
RD-0120: 1,520kN, 추중비 43.95 (진공 기준)


러시아쪽 LOX+LH2 엔진 중에선 그나마 SSME 추력 따라가네.

추력 1,961kN까지 나오는 진공 기준으로도 추중비가 거의 반토막이란 게 문제지만