0010110 rs2 rs1 011 rd 0101111 SC.W 00001 aq rl 00000 rs1 rm rd 1000011 FMADD.H rs3 10 rs2 rs1 001 rd 1010011 FSGNJ.Q 0010011 rs2 rs1 100 imm[4:0] 0100111 FSH rs3 10 rs2 rs1 rm rd 1010011 FMUL.S 0001100 rs2 rs1 110 rd 0110011 MULH 0000001 rs2 rs1 101 rd 0010011 SLTI imm[11:0] rs1 funct3 rd opcode I-type imm[11:5] rs2 rs1 000 rd 1010011 FCVT.WU.S 1110000 00000 rs1 000 rd 1010011 FMUL.H 0001110 rs2 rs1 rm rd 1000111 FMSUB.H rs3 10 rs2 rs1 rm rd 1010011 FEQ.Q 1010011 rs2 rs1 101 rd 0111011 DIVUW 0000001 rs2 rs1 rm rd 1010011 FCVT.Q.WU RV64Q Standard Extension 00010 aq rl rs2 rs1 rm rd 1010011 FMAX.D 0100000 00001 rs1 rm rd 1010011 FCVT.Q.LU 31 27 26 25 24 20 19 15 14 12 11 7 6 5 4 v4*n+3 7 6 5 4 3 2 VLEN=32b, SEW=16b, LMUL=4 Byte 3 2 1 0 0 m o "////'_ _////" <_1,5 xlO e I0 x I0 s) (NEWTONS) PROPULSION MODULE (Oz/H 2 ) Fig. 3.22--Lunar cargo shuttle ............................. 64 3. g3--Solid-propellant-boosted, earth-launched lunar logistic vehicle .................. 66 4. l--Saturn V with three exploration mission departure weight
roughened