IHI Aerospace Co. Ltd. / ISAS ----> JAXA |
M-3SI | M-3SII | M-V -I | M-V -II | ||||||
Overall Vehicle |
Operational | from | 17.02.1980 | 07.01.1985 | 12.02.1997 | 09.05.2003 | ||||
to | 14.02.1984 | 15.01.1995 | 10.02.2000 | 22.09.2006 | ||||||
Orbital flights | 4 | 8 | 3 | 4 | ||||||
Payload weight | t | M-3SI-1 | 0.185 | M-3SII-1 | 0.138 | GTO | 1.215 | GTO | 1.280 | |
Gross liftoff weight | t | 48.65 | 64.64 | 132.90 | 137.20 | |||||
Gross propellant weight | t | 38.09 | 49.34 | 114.58 | 118.42 | |||||
Total length | m | 23.80 | 27.78 | 30.80 | 30.80 | |||||
Max. diameter (span) | m | |||||||||
Total liftoff thrust (s.l.) | kN | 1,890.9 | 1,741.5 | 3,386.5 | 3,386.5 | |||||
Total impulse (vac) | MN*s | 99.9 | 129.6 | 315.0 | 326.5 | |||||
Fairing |
Total length | m | 4.00 | 6.85 | 9.19 | 9.19 | ||||
Diameter | m | 1.41 | 1.63 | 2.50 | 2.50 | |||||
Total weight | t | 0.30 | 0.52 | 0.70 | 0.70 | |||||
Stage 4 | Name | Nissan KM-P | Nissan KM-V1 | Nissan KM-V2a | ||||||
Length | m | 1.50 | 1.50 | |||||||
Diameter | m | 1.20 | 1.20 | |||||||
Liftoff weight | t | 0.653 | 1.430 | 3.000 | ||||||
Propellant weight | t | 0.606 | 1.312 | 2.500 | ||||||
Engines | ||||||||||
Propellant | solid HTPB | solid HTPB | solid HTPB | |||||||
Total thrust (vac) | kN | 52.0 | 81.3 | |||||||
Specific impulse (vac) | N*s/kg | 2922 | 2922 | |||||||
Burn time | s | 73.6 | 90 | |||||||
Total impulse (vac) | MN*s | 3.8 | 7.3 | |||||||
Stage 3 |
Name |
Nissan M-3A | Nissan M-3B | Nissan M-34a TVC | Nissan M-34b TVC | |||||
Length | m | 2.04 | 3.06 (2.66) | 2.97 | 3.61/4.29 | |||||
Diameter | m | 1.41 (1.14) | 1.62 (1.50) | 2.50 (2.16) | 2.50 (2.21) | |||||
Liftoff weight | t | 1.426 | 4.209 | 10.80 | 11.60 | |||||
Propellant weight | t | 1.084 | 3.298 | 10.03 | 10.80 | |||||
Engines | ||||||||||
Propellant | solid | solid | solid BP-205J | solid BP-205J | ||||||
Total thrust (vac) | kN | 56.9 | 132.0 | 294.2 (av) | 294.2 (av) | |||||
Specific impulse (vac) | N*s/kg | 2785 | 2874 | 2942 | 2942 | |||||
Burn time | s | 53.1 | 71.9 | 100.3 | 108 | |||||
Total impulse (vac) | MN*s | 3.0 | 9.5 | 29.5 | 31.8 | |||||
Stage 2 |
Name | Nissan M-22 TVC | Nissan M-23 TVC | Nissan M-24 TVC | Nissan M-25 TVC | |||||
Length | m | 4.89 | 6.27 | 7.88 (6.80) | 7.88 (6.61) | |||||
Diameter | m | 1.41 | 1.60 | 2.50 | 2.50 | |||||
Liftoff weight | t | 11.043 | 17.267 | 34.47 | 36.35 | |||||
Propellant weight | t | 7.201 | 10.317 | 31.06 | 32.94 | |||||
Engines | ||||||||||
Propellant | solid | solid | solid BP-204J | solid BP-208J | ||||||
Total thrust (vac) | kN | 324.6 | 524.6 | 1,239.0 (av) | 1,243.3 (av) | |||||
Specific impulse (vac) | N*s/kg | 2716 | 2765 | 2824 | 2834 | |||||
Burn time | s | 60.2 | 54.4 | 70.8 | 74.9 | |||||
Total impulse (vac) | MN*s | 19.6 | 28.5 | 87.7 | 93.4 | |||||
Stage 1 |
Name | Nissan M-13 TVC | Nissan M-13 TVC | Nissan M-14 TVC | Nissan M-14 TVC | |||||
Length | m | 14.91 | 14.66 | 13.73 | 13.73 | |||||
Diameter | m | 1.41 | 1.41 | 2.50 | 2.50 | |||||
Liftoff weight | t | 31.60 | 31.60 | 84.26 | 84.26 | |||||
Propellant weight | t | 27.064 | 27.098 | 72.18 | 72.18 | |||||
Engines | ||||||||||
Propellant | solid | solid | solid BP-204J | solid BP-204J | ||||||
Total thrust (s.l.) | kN | 1,134.3 | 1,134.3 | 3,386.5 | 3,386.5 | |||||
Specific impulse (s.l.) | N*s/kg | 2344 | 2344 | 2393 | 2393 | |||||
Burn time | s | 55.9 | 56.0 | 51 | 51 | |||||
Total impulse (vac) | MN*s | 70.6 | 70.7 | 194.0 | 194.0 | |||||
Booster |
Name | 8 SB-310 | 2 SB-735 TVC | |||||||
Length | m | 5.79 | 9.14 | |||||||
Diameter | m | 0.31 | 0.74 | |||||||
Liftoff weight | t | 4.119 | 10.248 | |||||||
Propellant weight | t | 2.741 | 8.023 | |||||||
Engines | ||||||||||
Propellant | solid | solid | ||||||||
Total thrust (s.l.) | kN | 756.6 | 607.2 | |||||||
Specific impulse (s.l.) | N*s/kg | 2148 | 2344 | |||||||
Burn time | s | 7.8 | 31.0 | |||||||
Total impulse (vac) | MN*s | 6.7 | 20.9 |