Credit: NASDA. 16,821 bytes. 195 x 330 pixels.
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| MV-1B - Credit: NASDA. 16,821 bytes. 195 x 330 pixels. |
 | Launch Vehicle: L-4S. First Japanese orbital launch vehicle. |
 | Launch Vehicle: Mu-3S. |
 | Launch Vehicle: H-1. |
 | Launch Vehicle: H-2. |
| Launch Vehicle: J-1. All-solid rocket motor launch vehicle. Because of the high cost, an alternate J-1 F2 design was developed. |
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| Launch Vehicle: M-V. All-solid satellite launch vehicle. |
| Launch Vehicle: H-2 HIMES. |
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| Launch Vehicle: H-2A 2024. Low-cost version of H-2 developed for the commercial market. The two SRB-A solid rocket boosters can be supplemented by 4 smaller SSB solid boosters. 0 or 2 SSB's can be fitted for reduced 9,940 kg or 10,740 kg LEO payloads. |
| Launch Vehicle: J-1 F2. All-solid rocket motor launch vehicle. Lower cost alternate to the original J-1 design. Uses the SRB-A of the H-2A vehicle as the first stage, the second and third stages of the J-1, with updated avionics. |
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| Launch Vehicle: H-2A 212. Low-cost version of H-2 developed for the commercial market. This version uses two core stages side-by-side in an asymmetric configuration, supplemented by two SRB solid rocket boosters. |