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SRB-A

Family of Japanese solid rocket boosters From Wikipedia, the free encyclopedia

SRB-A
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The SRB-A and SRB-3 are a family of Japanese solid-fueled rocket boosters developed and manufactured by IHI Corporation for use on the H-IIA, H-IIB, Epsilon, H3, and Epsilon S launch vehicles. The earlier versions, designated SRB-A, flew from 2001 to 2025, while the successor SRB-3 made its first flight in 2023.

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Design

All SRB variants have a composite motor case constructed from carbon-fiber-reinforced polymer materials, with thrust vector control provided by electrically actuated nozzles. IHI led development and production, with contributions from other Japanese manufacturers: the composite propellant (BP-208) was developed by NOF Corporation, and the T1000GB carbon fiber used in the motor case was developed by Toray.[3]

The SRB-A motor case incorporated foreign technology licensed from Alliant Techsystems (ATK), based on the Castor 120 motor used in the LGM-118 Peacekeeper ICBM.[4] By contrast, the SRB-3 uses a fully domestic motor case design developed in Japan.[5]

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SRB-A series

The SRB-A was developed for the H-IIA rocket and first flew in 2001. It was later used on the larger H-IIB and as the first stage of the smaller Epsilon rocket. It measured 2.5 metres (8 ft 2 in) in diameter and 15.1 metres (50 ft) in length, with a filament-wound composite casing. It replaced the SRBs used on the earlier H-II rocket.[6]

Variants

  • SRB-A — The initial version, used on the first six H-IIA launches. A separation failure on the sixth launch in 2003 led to loss of mission.[6][7]
  • SRB-A2 — A planned upgrade canceled after the 2003 failure; its design changes were merged into the SRB-A Improved.
  • SRB-A Improved — Incorporated a redesigned bell-shaped nozzle to reduce erosion, with slightly lower thrust and longer burn time. Used on the seventh through thirteenth H-IIA flights, but nozzle erosion persisted.
  • SRB-A3 — Final SRB-A version, with further improvements to reliability and performance. Available in a high-thrust or long-burn variant. Used on all H-IIA launches after the thirteenth flight, as well as on the H-IIB and as the first stage of the Epsilon rocket.[6][8][9]

The SRB-A series was retired in 2025 and replaced by the SRB-3.

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SRB-3

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Closeup of SRB-3 models attached to a model H3 rocket

The SRB-3 is the current generation of Japanese solid rocket boosters, developed for the H3 and Epsilon S launch vehicles. Compared to the SRB-A, it carries 1 tonne (2,200 lb) more propellant, uses a fixed nozzle, and incorporates a simplified separation system to reduce cost and increase reliability.[5][10]

Unlike the SRB-A series, which required different burn patterns depending on configuration and vehicle type, the SRB-3 uses a unified burn pattern whether flown in pairs or quartets on the H3, or as the first stage of the Epsilon S.[10]

References

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