Table V. (Continued). Mars piloted vehicle Isp (sec): MPS: 460.0 RCS: 220.0 B/O rate (kg/day): 5.1 Reserves (%): MPS: 2 RCS: 10 Phobos payload: 0 Stage: 60 864 Brake: 8215 Deimos payload: 0 Sample return: 100 Sequential weight Delta V (M/S) Time MPS fluids RCS Mission event MPS RCS days boiloff Nominal fluids other kg lb TMIS separation 99 377 219087 Earth-to-Mars transfer 0 0 200 -1023 0 0 -1023 -2256 Mars aeromaneuver weight 98 354 216 830 MPS Phobos rendezvous 575 0 0 0 -11 770 0 -11 770 -25 949 Drop Phobos payload 0 0 0 0 0 0 0 0 0 Mars orbit staytime 0 0 365 -1868 0 0 -1868 -4117 MPS Deimos rendezvous 0 0 0 0 0 0 0 Drop Deimos payload 0 0 0 0 0 0 0 0 0 Add sample return 0 0 0 0 0 0 100 100 220 MPS rendezvous with TEIS 635 0 0 0 -11 137 0 -11 137 -24 552 TEIS rendezvous weight 73 679 162 432 Mars to Earth transfer 0 0 200 -1023 0 0 100 -923 -2036 Earth aeromaneuver weight 72 755 160397 MPS post aero correction 200 0 0 0 -3155 0 -3155 -6956 Less aerobrake 0 0 0 0 0 0 -8215 -8215 -18111 MPS reserves 0 0 0 0 -521 -521 -1149 End of mission, excluding reserves 60 864 134181 Total 1410 0 765 0 -3914.3 -26 062 0 0 -8536 Fluid reserves -521 0 Total usable fluid weight—kg | -30498 | 0___ 1
RkJQdWJsaXNoZXIy MTU5NjU0Mg==