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KBKhA RD-0410 nuclear-thermal rocket engine

KBKhA's RD-0410 (11B91) was a Soviet experimental nuclear-thermal rocket engine using liquid hydrogen as the working propellant. NASA's nuclear-thermal propulsion materials place the RD-0410 engine program in 1970–1986; Russian Academy material identifies 11B91 as KBKhA-developed, and a technical KBKhA history records 1988 testing of the nuclear engine. This historical ground-test identity is retained as retired with no flight installation asserted.

Identity

Aliases
RD0410РД-041011B9111Б91
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
KBKhA RD-0410 nuclear-thermal rocket engine
Status
retired

Details

Description
KBKhA's RD-0410 (11B91) was a Soviet experimental nuclear-thermal rocket engine using liquid hydrogen as the working propellant. NASA's nuclear-thermal propulsion materials place the RD-0410 engine program in 1970–1986; Russian Academy material identifies 11B91 as KBKhA-developed, and a technical KBKhA history records 1988 testing of the nuclear engine. This historical ground-test identity is retained as retired with no flight installation asserted.
Developers
Propellants
liquid hydrogen
Rocket Specs
Cycle
nuclear thermal
Vacuum Thrust Kn
35.3

Links

Assets & Meta

Creation Time
August 15, 2026 at 03:54:07 UTC
Updated Time
August 15, 2026 at 03:54:07 UTC

Other

Sources
  • Accessed Date
    2026-08-14
    Note
    NASA nuclear-thermal propulsion material identifies the RD-0410 engine program as a 1970–1986 Russian effort using advanced ceramic fuel technology.
    Publisher
    NASA Technical Reports Server
    Title
    Nuclear Thermal Rocket Fuel Development
  • Accessed Date
    2026-08-14
    Note
    Russian Academy material identifies the 11B91 (RD-0410) nuclear-thermal engine as developed at KBKhA in the USSR.
    Publisher
    Russian Academy of Sciences
    Title
    Nuclear rocket engines and nuclear rocket power systems
  • Accessed Date
    2026-08-14
    Note
    The KBKhA technical history records 1988 tests of the nuclear RD-0410 and reports approximately 35.3 kN thrust; this is the only entered numeric rating and is kept narrow to the reported test value.
    Publisher
    Aerospace Engines A to Z
    Title
    KBKhA engine specifications