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Created by hedgehog on 9/4/2007

RD-0410 ^en

mid: /m/0523nd9 notable type: /spaceflight/rocket_engine notable for: /spaceflight/rocket_engine on the web: wikipedia.org

RD-0410 was a Soviet nuclear thermal rocket engine developed from 1965 through the 1980s using liquid hydrogen propellant. The engine was ground-tested at the Semipalatinsk Test Site, and its use was incorporated in the Kurchatov Mars 1994 manned mission proposal. The hydrogen boost turbopump was designed by KBKhA. Wikipedia [ - ]

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Rocket engine
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#9202a8c04000641f800000000a21d189

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RD-0410

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Key /type/object/key

Timestamp /type/object/timestamp

Tuesday, September 04, 2007 12:17 PM

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/boot/all_permission

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hedgehog

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hedgehog

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/m/0523nd9

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Description /common/topic/description

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RD-0410 was a Soviet nuclear thermal rocket engine developed from 1965 through the 1980s using liquid hydrogen propellant. The engine was ground-tested at the Semipalatinsk Test Site, and its use was incorporated in the Kurchatov Mars 1994 manned mission proposal. The hydrogen boost turbopump was designed by KBKhA. Wikipedia

2 values total »

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http://www.popmech.ru/part/print.php?rubricid=13&articleid=1523

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RD-0410 (РД-0410, GRAU index: 11B91) was a Soviet nuclear thermal rocket engine developed from...

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Rocket engine

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Monday, May 20, 2013 8:58 PM

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Status /spaceflight/rocket_engine/status

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Used in rocket stages /spaceflight/rocket_engine/used_in_rocket_stages

Rocket	Stage Number	Number Of Engines	Thrust	Burn Time	Fuels
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Government designation /spaceflight/rocket_engine/government_designation

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Manufactured by /spaceflight/rocket_engine/manufactured_by

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Designed by /spaceflight/rocket_engine/designed_by

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Design period /spaceflight/rocket_engine/design_period

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Use period /spaceflight/rocket_engine/use_period

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Diameter /spaceflight/rocket_engine/diameter

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Height /spaceflight/rocket_engine/height

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Thrust (vacuum) /spaceflight/rocket_engine/thrust_vacuum

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Thrust (sea level) /spaceflight/rocket_engine/thrust_sea_level

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Isp (vacuum) /spaceflight/rocket_engine/isp_vacuum

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Isp (sea level) /spaceflight/rocket_engine/isp_sea_level

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Dry mass /spaceflight/rocket_engine/dry_mass

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Throttle ratio /spaceflight/rocket_engine/throttle_ratio

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Used in rocket stages /user/hedgehog/default_domain/rocket_engine/used_in_rocket_stages

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Goverment designation /user/hedgehog/default_domain/rocket_engine/goverment_designation

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11B91

Manufactured by /user/hedgehog/default_domain/rocket_engine/manufactured_by

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Designed by /user/hedgehog/default_domain/rocket_engine/designed_by

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Design period /user/hedgehog/default_domain/rocket_engine/design_period

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Use period /user/hedgehog/default_domain/rocket_engine/use_peiod

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Diameter /user/hedgehog/default_domain/rocket_engine/diameter

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Height /user/hedgehog/default_domain/rocket_engine/height

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Thrust (vacuum) /user/hedgehog/default_domain/rocket_engine/thrust_vacuum

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Thrust (sea level) /user/hedgehog/default_domain/rocket_engine/thrust_sea_level

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Isp (vacuum) /user/hedgehog/default_domain/rocket_engine/isp_vacuum

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Isp (sea level) /user/hedgehog/default_domain/rocket_engine/isp_sea_level

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Dry mass /user/hedgehog/default_domain/rocket_engine/dry_mass

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Reactor fuel /user/hedgehog/default_domain/solid_core_nuclear_thermal_engine/reactor_fuel

Enriched uranium

Reactor power /user/hedgehog/default_domain/solid_core_nuclear_thermal_engine/reactor_power

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Expansion ratio /user/hedgehog/default_domain/solid_core_nuclear_thermal_engine/expansion_ratio

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Chamber pressure /user/hedgehog/default_domain/solid_core_nuclear_thermal_engine/chamber_pressure

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Propellant /user/hedgehog/default_domain/solid_core_nuclear_thermal_engine/propellant

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Projects /projects/project_focus/projects

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Category /engineering/engine/category

Rocket engine

Mass /engineering/engine/mass

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Output Power /engineering/engine/power

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Energy source /engineering/engine/energy_source

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First Ran /engineering/engine/first_ran

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Designer /engineering/engine/designer

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Variants /engineering/engine/variants

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Thrust /engineering/reaction_engine/thrust

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35.2 kN

Specific fuel consumption /engineering/reaction_engine/specific_fuel_consumption

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Specific impulse /engineering/reaction_engine/specific_impulse

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article /base/engineeringdraft/topic/article

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Category /base/engineeringdraft/manufactured_component/category

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Components (Meronyms) /base/engineeringdraft/manufactured_component/meronyms

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Variation of /base/engineeringdraft/manufactured_component/variation_of

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Instance /base/engineeringdraft/manufactured_component/instance

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Material Composition by Mass /base/engineeringdraft/manufactured_component/material_composition_by_mass

Material	Mass
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First introduced /base/engineeringdraft/manufactured_component/first_introduced

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Introduced by /base/engineeringdraft/manufactured_component/introduced_by

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Manufactured by /base/engineeringdraft/manufactured_component/manufactured_by

Manufacturer	Plant	From	To
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Factory production records /base/engineeringdraft/manufactured_component/production_records

Factory	Volume	From	To
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Total produced /base/engineeringdraft/manufactured_component/total_produced

number	date	Source
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End of production /base/engineeringdraft/manufactured_component/end_of_production

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