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Rocket Engine, Liquid Fuel, S-3D for Jupiter Missile

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
HAZ MAT: Asbestos
HAZ MAT: Thoriated Magnesium
Ferrous Alloy
Aluminum Alloy
Rubber
Copper Alloy
Electrical Wiring
Dimensions:
3-D (Approximate): 398.8 × 190.5 × 205.7cm (13 ft. 1 in. × 6 ft. 3 in. × 6 ft. 9 in.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1958
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700262000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700262000

Rocket Engine, Liquid Fuel, J-2

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Stainless steel and other metals.
Dimensions:
Overall: 11 ft. × 6 ft. 8 3/8 in., 5740lb. (335.3 × 204.2cm, 2603.6kg)
3-D (Dimensions on stand): 365.8 × 205.7 × 243.8cm (12 ft. × 6 ft. 9 in. × 8 ft.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1964
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700261000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700261000
Additional Online Media:

Rocket Engine, Liquid Fuel, F-1

Title:
F-1 Engine
Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Cooling tubes (178 tubes), Inconel X; injector, stainless steel and copper; propellant lines, aluminum; valves, aluminum and stainless steel
Dimensions:
Overall: 18 ft. 4 15/16 in. long x 12 ft. 5/16 in. diameter, 18340 lb. (561.24 x 366.52cm, 8319kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1963
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700271000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700271000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furanced brazed.
Dimensions:
Overall: 8 ft. 4 in. long x 3 ft. 11 in. diameter (254 x 119.38cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1975
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700257000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700257000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1A

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages: 347 stainless steel. Propellant tanks, lines, and valves: stainless steel. Pumps: aluminum alloys; turbine: Hastealloy. Injector: OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 100 in. long x 47 in. diameter (254 x 119.38cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1963
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700286000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700286000
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Model, Rocket Engine, Liquid Fuel, J-2, 1:8 Scale

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Plastic, paint, lucite, metal, wood,
Dimensions:
Overall: 1 ft. 1 1/2 in. long x 7 1/2 in. diameter (34.29 x 19.05cm)
Type:
MODELS-Propulsion
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19740738000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19740738000
Additional Online Media:

Rocket Engine, Liquid Fuel, F-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Cooling tubes (178 tubes), Inconel X; injector, stainless steel and copper; propellant lines, aluminum; valves, aluminum and stainless steel
Dimensions:
Overall: 220 15/16 in. long x 144 5/16 in. diameter, 18340 lb. (561.24 x 366.52cm, 8319kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19751448000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19751448000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 100 in. long x 47 in. diameter (254 x 119.38cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1975
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19800474000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19800474000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 5 ft. 3/8 in. wide x 6 ft. 1 1/4 in. long x 3 ft. 11 in. diameter, 2000 lb. (153.42 x 186.06 x 119.38cm, 907.2kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1975
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19680012000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Location:
Steven F. Udvar-Hazy Center in Chantilly, VA
Exhibit Station:
Rockets & Missiles
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19680012000

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 8ft 4in. x 3ft 11in., 1532lb. (2,300 lbs in crate) (254 x 119.38cm, 694.9kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1969
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700255000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700255000

Rocket Engine, Liquid Fuel, H-1A

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Steel combustion chamber; some aluminum alloy
Dimensions:
Length, 100 inches; diameter, outside, nozzle, 47 inches; width 70 inches; weight, 1,820 pounds
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1969
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700256000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700256000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 100 in. tall x 47 in. diameter (254 x 119.38cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1969
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700258000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700258000

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dessicant holders on each side of rocket plumbing, with red plastic protective covers; bundle of wires in white plastic isulation adjacent to red desicant holders; another bundle of wires with white plastic insulation, in back of plumbing,
Dimensions:
Overall: 5ft 3 1/2in. x 4ft 5 3/4in. x 8ft 4in. (161.3 x 136.5 x 254cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1959-1961
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700259000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700259000

Handler, Rocket Engine, Liquid Fuel, F-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Overall: Steel
Tire rims: Non-ferrous
Tires: Hardened rubber
Dimensions:
Length: 182.75 inches
Width: 142 inches
Height, maximum, with struts: 72 inches
Height of floor level beams: 28.5 inches
Weight: 5,500 lbs.
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700271001
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700271001

Rocket Engine, Liquid Fuel, H-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 75 in. tall x 98 in. long x 47 in. diameter, 1870 lb. (190.5 x 248.92 x 119.38cm, 848.2kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1975
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700284000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700284000
Additional Online Media:

Rocket Engine, Liquid Fuel, H-1, Cutaway

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dimensions:
Overall: 8 ft. 4 in. long x 3 ft. 11 in. diameter (254 x 119.38cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1958-1969
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19700285000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19700285000

Injector Head, Rocket Engine, Liquid Fuel, Lunar Module Ascent Engine

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Aluminum, Ink
Dimensions:
Overall (Injector Head): 11in. x 2 1/8in. (27.94 x 5.4cm)
Overall (Cover): 11 1/2in. x 6 1/2in. (29.21 x 16.51cm)
Type:
PROPULSION-Components (Engine Parts)
Country of Origin:
United States of America
Credit Line:
Transferred to the National Air and Space Museum from the National Aeronautics and Space Administration
Inventory Number:
A19731212000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19731212000
Additional Online Media:

Rocket Engine, Liquid Fuel, F-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Cooling tubes (178 tubes), Inconel X; injector, stainless steel and copper; propellant lines, aluminum; valves, aluminum and stainless steel
Dimensions:
Overall: 220 15/16 in. length x 144 5/16 in. diameter (561.24 x 366.52 cm)
Approximate: 18340 lb. (8319 kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19750649000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19750649000
Additional Online Media:

Rocket Engine Turbo Pump, Cutaway, F-1

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Inlets, volutes, and impellers, aluminum alloy casting. Turbine wheels and manifold assemblies, nickel alloy.
Dimensions:
Overall: 5 ft. 2 in. tall x 4 ft. wide, 2000 lb. (w/Crate 2,500lb.) (157.48 x 121.92cm, 907.2kg)
Type:
PROPULSION-Components (Engine Parts)
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19751580000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19751580000

Rocket Engine, Liquid Fuel, Vernier, Atlas Missile

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Overall, steel; aluminum piping; plastic protective cap over nozzle
Dimensions:
Overall: 2 ft. wide x 2 ft. 7 in. long, 47 lb. (60.96 x 78.74cm, 21.3kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1963
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19761839000
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum
See more items in:
National Air and Space Museum Collection
Location:
Steven F. Udvar-Hazy Center in Chantilly, VA
Exhibit Station:
Rockets & Missiles
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19761839000

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