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Expendable LV's

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Angara
Ariane 4
Ariane 5
Athena
Atlas II
Atlas III
Atlas V
Avrora (Aurora)
Beal BA-2
Delta II
Delta III
Delta IV
Dnepr
Eurockot
GSLV
H-IIA
J-1
Kosmos 3M
Long March 3
Pegasus
Proton
Shtil
Soyuz
Start
Strela
Taurus
Titan II
Titan IV
Tsiklon
Zenit

   H-IIA - Image 2
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h2a_modificate.gif (16580 bytes)H-IIA Flight Sequence

Fairing: simplified design, simplified manufacturing
Avionics:  box integration, HIC parts application, simplified interface (data bus), automatic check-out support function.
Second Stage:  eliminated LOX / LH2 common bulkhead, LE-5B engine (improved LE-5A), simplified propulsion system.
First Stage:  simplified manufacturing, new core / SRB-A / core stage support concept, simplified propulsion system, LE-7A engine (improved LE-7), modification of the rigging and simplification of the system, increase casting and machining.
Solid Rocket Booster:  one-segment CFRP motor case, miniaturized nozzle, electromechanical TVC system.


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