7 TEXT:HOME 10 REM PRINT CHR$(4);"BLOAD GLOBE.HGR,A$2000" 20 AN$="ZURGTROYD" 90 S=3 95 G=-9.8 100 EN(1)=1:ST(1)=1:FT(1)=1 101 EN(2)=2:ST(2)=2:FT(2)=1 102 EN(3)=3:ST(3)=3:FT(3)=1 103 LN=0 104 CQ=0 110 HIMEM:7925 120 POKE 232,245:POKE 233,30 130 FOR L=7925 TO 8175: READ B:POKE L,B:NEXT L 1000 PRINT "ROCKET SUMMARY:":PRINT 1005 FOR I=1 TO S 1010 EM(I)=EN(I)*1.5+ST(I)*FT(I)*0.5 1012 IF I=1 THEN EM(I)=EM(I)+1.0 1014 FM(I)=ST(I)*FT(I)*4.0 1015 SF(I)=FM(I) 1016 SM(I)=EM(I)+FM(I) 1020 TM(I)=0 1022 FOR J=1 TO I 1025 TM(I)=TM(I)+SM(J) 1030 NEXT J 1035 TH(I)=EN(I)*168 1040 DV(I)=270*-G*LOG(TM(I)/(TM(I)-FM(I))) 1050 TW(I)=TH(I)/(TM(I)*-G) 1055 FF(I)=TH(I)/(270*-G) 1990 PRINT "STAGE: ";I 1991 PRINT " TANKS=";ST(I)*FT(I);" ENGINES=";EN(I) 1992 PRINT " STAGE MASS=";SM(I);" TOTAL MASS=";TM(I) 1993 PRINT " DELTAV=";DV(I) 1995 PRINT " TWR=";TW(I) 2000 NEXT I 2999 GET A$ 3000 AN=0 3012 GX=0:GY=-9.8:GA=0 3013 V=0:VX=0:VY=0 3014 AX=0:AY=0 3015 KR=600000 3016 RX=0:RY=KR+10 3017 RA=KR+10 3018 TR=0:T=0 3020 HGR:ROT=0:SCALE=2:H=0 3030 REM ** LAUNCHPAD ** 3035 PRINT:PRINT CHR$(4);"BLOAD LAUNCHPAD.HGR,A$2000" 3038 HCOLOR=1:HPLOT 1,80 TO 132,80: HPLOT 148,80 TO 247,80 3039 HCOLOR=3:HPLOT 110,110 TO 110,60:HPLOT TO 130,60: HPLOT 110,70 TO 130,70 4000 REM 4001 IF LN=0 GOTO 5032 4003 IF (RA-KR)>1800 THEN GOTO 4012 4005 HCOLOR=0:HPLOT 1,80+H TO 132,80+H:HPLOT 148,80+H TO 247,80+H 4010 H=(RA-KR)/20:HCOLOR=1:HPLOT 1,80+H TO 132,80+H:HPLOT 148,80+H TO 247,80+H 4012 IF (RA-KR)<10000 AND CQ<>0 THEN GOSUB 7600 4014 IF (RA-KR)<10000 GOTO 4018 4016 IF (RA-KR)>10000 AND CQ<>1 THEN GOSUB 7700 4018 FL=FM(S)*100/SF(S) 4020 IF TR<>1 THEN GOTO 4050 4025 IF FM(S)<0.1 THEN FM(S)=0:AX=0:AY=0:GOTO 4050 4030 AX=(TH(S)/TM(S))*SIN(AN) 4035 AY=(TH(S)/TM(S))*COS(AN) 4040 FM(S)=FM(S)-FF(S) 4045 TM(S)=TM(S)-FF(S) 4047 GOTO 4060 4050 REM NOT THRUSTING 4055 AX=0:AY=0 4060 GA=ATN(RX/RY) 4062 REM PRINT "GA=";GA;" AY=";AY 4065 IF RY<0 THEN GA=GA+3.14 4070 GY=COS(GA)*G 4075 GX=SIN(GA)*G 4080 AY=AY+GY 4085 AX=AX+GX 4090 ZX=VX 4095 ZY=VY 5000 VY=ZY+AY 5005 VX=ZX+AX 5010 V=SQR(VX*VX+VY*VY) 5012 RY=RY+0.5*(ZY+VY) 5014 RX=RX+0.5*(ZX+VX) 5018 RA=SQR(RX*RX+RY*RY) 5020 IF RA