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Rocket Engines, Liquid Fuel, Dual XLR-11 (X-15 Interim Engine Pair)

Manufacturer:
Reaction Motors, Inc.  Search this
Materials:
Mainly stainless steel, some titanium, some copper alloy tubing; pump housing, cast aluminum; insulated electrical wiring.
Dimensions:
Length, 82 inches; width, 42 inches; height, 48 inches; length, thrust cylinders (8), 21.75 inches each; diameter, cylinders (8), 6 inches each; weight, approximately 500 pounds (empty weight of each XLR-11 is 210 pounds).
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1959-1961
Credit Line:
Transferred from the U.S. Air Force
Inventory Number:
A19630364000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9b7e16d7e-8f31-419d-8fe0-37157275b184
EDAN-URL:
edanmdm:nasm_A19630364000

Rocket Engines, Liquid Fuel, XLR-11, Dual (Interim X-15 Pair)

Manufacturer:
Reaction Motors, Inc.  Search this
Materials:
Mainly stainless steel, some titanium, some copper alloy tubing; pump housing, cast aluminum; insulated electrical wiring.
Dimensions:
Length, 82 inches; width, 42 inches; height, 48 inches; length, thrust cylinders (8), 21.75 inches each; diameter, cylinders (8), 6 inches each; weight, approximately 500 pounds (empty weight of each XLR-11 is 210 pounds),
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Gift of the Air Force.
Inventory Number:
A19630365000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv984c576b6-ac3e-4d0d-b867-ef2a2dbde07f
EDAN-URL:
edanmdm:nasm_A19630365000

Rocket Engines, Liquid Fuel, Attitude and Roll Control, Titan 3E Launch Vehicle

Manufacturer:
Rocketdyne, Division of North American Aviation Co.  Search this
Materials:
Phenolic Resin
Anodized Aluminum
Aluminum
Plastic
Adhesive
Rubber
Ink
Steel
Dimensions:
3-D: 49.5 × 41.9 × 14cm (19 1/2 × 16 1/2 × 5 1/2 in.)
Storage: 59.7 × 52.1 × 24.1cm (23 1/2 × 20 1/2 × 9 1/2 in.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1967
Credit Line:
Transferred from U.S. Air Force - Patrick AFB
Inventory Number:
A19700335000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv93a41e972-6fcc-49ac-b485-f93ab2d43e67
EDAN-URL:
edanmdm:nasm_A19700335000
Online Media:

Rocket Engine, BMW 109-558

Manufacturer:
BMW (Bayerische Motoren Werke)  Search this
Materials:
Steel nozzle
Dimensions:
Approximate (outside nozzle diameter): 3 1/4in. x 1ft 6in. (8.26 x 45.72cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
Germany
Credit Line:
Transferred from the U.S. Air Force
Inventory Number:
A19603382001
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9d4b3915d-8a08-45a8-88a3-a1802fc0d1e3
EDAN-URL:
edanmdm:nasm_A19603382001
Online Media:

Valve, Rocket Engine, Monopropellant

Manufacturer:
Hydraulic Research & Manufacturing Co., Inc.  Search this
Materials:
Steel, stainless steel, anodized aluminum, plastic, adhesive label
Dimensions:
Approximate: 8.9 x 7 x 6.4cm (3 1/2in. x 2 3/4in. x 2 1/2in.)
Type:
PROPULSION-Accessories (to an Engine)
Country of Origin:
United States of America
Credit Line:
Gift of Thiokol Chemical Corporation
Inventory Number:
A19771257000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9310e0ea5-7f0a-4f3c-806d-d9d19e2a0784
EDAN-URL:
edanmdm:nasm_A19771257000

Rocket Engine, Liquid Fuel, D50C1

Manufacturer:
Reaction Motors, Inc.  Search this
Materials:
Copper Alloy
Paint
Steel
Dimensions:
3-D: 38.1 x 20.3 x 5.1cm (15 x 8 x 2 in.)
Storage: 22.9 x 40.6 x 8.9cm (9 in. x 16 in. x 3 1/2 in.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Reaction Motors Division, Thiokol Chemical Corp.
Inventory Number:
A19850117000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9480e5b73-6f9d-4113-83ab-ff760a91794d
EDAN-URL:
edanmdm:nasm_A19850117000

Rocket Engine, Vernier, Surveyor Spacecraft

Manufacturer:
Reaction Motors Div., Thiokol Chemical Corp.  Search this
Materials:
Stainless steel; gold coating over plumbing
Dimensions:
Overall: 13 1/4 in. long x 5 1/4 in. diameter (33.66 x 13.34cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the NASA - Jet Propulsion Laboratory
Inventory Number:
A19790173000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9ecc79b52-735e-40e8-bc12-3e632f578028
EDAN-URL:
edanmdm:nasm_A19790173000
Online Media:

Section, Rocket Engine, NERVA

Manufacturer:
Aerojet Electrosystems Inc.  Search this
Materials:
Stainlless steel, high grade
Dimensions:
Overall: 3 in. tall x 7 1/4 in. wide x 7 in. deep (7.6 x 18.42 x 17.8cm)
Type:
PROPULSION-Components (Engine Parts)
Country of Origin:
United States of America
Credit Line:
Gift of Aerojet Nuclear Systems Company
Inventory Number:
A19731001004
Restrictions & Rights:
Usage conditions apply
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
GUID:
http://n2t.net/ark:/65665/nv96a98cdfd-d33b-431a-9d55-80c467abbbe3
EDAN-URL:
edanmdm:nasm_A19731001004
Online Media:

Liner, Rocket Engine, JATO, M17G

Manufacturer:
Reaction Motors, Inc.  Search this
Materials:
Steel
Copper
Phosphate surface finish
Foam
Adhesive
Dimensions:
14 7/8" x 6 15/16" Diameter
Type:
PROPULSION-Components (Engine Parts)
Country of Origin:
United States of America
Credit Line:
Reaction Motors Div., Thiokol Chemical Corp.
Inventory Number:
A19850107000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv97dce3aff-6192-40f1-98f6-90caf5bcd739
EDAN-URL:
edanmdm:nasm_A19850107000

Nozzle, Rocket Engine, Liquid Fuel

Manufacturer:
Reaction Motors, Inc.  Search this
Materials:
Copper
Dimensions:
Length, 4.25 inches; diameter, 4 inches; weight, about two pounds
(interior diameter at top of nozzle: 3 inches; interior diameter at bottom of nozzle: 2 inches)
Type:
PROPULSION-Miscellaneous
Country of Origin:
United States of America
Credit Line:
Gift of Reaction Motors Division, Thiokol Chemical Corporation
Inventory Number:
A19771256000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9dc99a8dc-cfe6-4a78-b7f6-786f06ef589b
EDAN-URL:
edanmdm:nasm_A19771256000
Online Media:

Rocket Engine, Liquid Fuel, for Jupiter Missile

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Primarily stainless steel; some aluminum piping
Dimensions:
Overall: 68 in. diameter x 120 in. long, approximate weight 4400 lb. (172.72 cm. diameter x 304.8 cm, long approximate weight 1995.8 kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1956-1963
Credit Line:
Transferred from NASA/Marshall Space Flight Center
Inventory Number:
A19700263000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv906818cfe-8efd-4294-8ccc-84c0227e40ab
EDAN-URL:
edanmdm:nasm_A19700263000

Rocket Engine, Liquid-Fuel, Cutaway, R.H. Goddard

Manufacturer:
Dr. Robert H. Goddard  Search this
Materials:
Steel, overall
Dimensions:
Overall: 2 ft. 11 3/4 in. long x 8 in. wide x 6 in. diameter (90.81 x 20.32 x 15.24cm); diameter, outside, nozzle, 4 inches
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Found in Collection
Inventory Number:
A19660023000
Restrictions & Rights:
Usage conditions apply
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
GUID:
http://n2t.net/ark:/65665/nv97c89a912-3d3e-4b44-bff6-d32168fba86a
EDAN-URL:
edanmdm:nasm_A19660023000

Rocket Engine, Liquid Fuel, V-2, U.S.-Made

Manufacturer:
North American Aviation Inc.  Search this
Materials:
Steel, Paint, Aluminum, Cadmium Plating, Mylar (Polyester), Adhesive, Asbestos, Plastic, Phenolic Resin,
Rubber (Silicone)
Dimensions:
Storage (Artex Crate): 325.1 × 160 × 170.2cm (10 ft. 8 in. × 63 in. × 67 in.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1947-1949
Credit Line:
Rocketdyne, Division of Rockwell International Corporation
Inventory Number:
A19700251000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv93bf3b7e6-3f8a-4356-898f-e286e158c685
EDAN-URL:
edanmdm:nasm_A19700251000
Online Media:

Rocket Engine, Liquid Fuel, Navaho Missile

Manufacturer:
North American Aviation Inc.  Search this
Materials:
Titanium alloys, stainless steel, and other metals.
Dimensions:
Overall: 6 ft. 7 in. tall x 6 ft. 4 in. wide x 8 ft. 9 in. long (200.66 x 193.04 x 266.7cm)
Other (Chamber): 5 ft. 5 1/2 in. diameter (166.37cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
1951-1956
Credit Line:
Gift of Rocketdyne, Division of North American Aviation Co.
Inventory Number:
A19700250000
Restrictions & Rights:
CC0
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
GUID:
http://n2t.net/ark:/65665/nv93abcdcfa-2051-4e9b-81dc-edbe57c467d6
EDAN-URL:
edanmdm:nasm_A19700250000
Online Media:

Rocket Engine, Liquid Fuel, A-4, Redstone Missile

Manufacturer:
Rocketdyne Division, Rockwell International Corporation  Search this
Materials:
Combustion chamber, injectors, and some tubing, 4130 steel; propellant lines, pumps, impellers, and valves, aluminum alloys including heat exchanger; harness manifold and other parts, steel.
Dimensions:
Other (outer): 2 ft. 8 in. diameter x 10 ft. 9 in. long x 4 ft. 1 in. wide (81.3 x 327.7 x 124.5cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the U.S. Army.
Inventory Number:
A19910078000
Restrictions & Rights:
Usage conditions apply
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
GUID:
http://n2t.net/ark:/65665/nv9afbd8370-50f9-4088-a416-eae1ea7089a0
EDAN-URL:
edanmdm:nasm_A19910078000

Rocket Engine, Combustion Chamber, V-2

Manufacturer:
Linke-Hofmann Werke AG  Search this
Materials:
Overall, steel
Dimensions:
Overall: 6ft 2in. x 3ft 7in. (187.96 x 109.22cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
Germany
Credit Line:
Transferred from the U.S. Air Force
Inventory Number:
A19730004000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv96172300c-44c4-4c85-a8b1-4900cbfb572d
EDAN-URL:
edanmdm:nasm_A19730004000
Online Media:

Rocket Engine, Combustion Chamber, V-2

Manufacturer:
Linke-Hofmann Werke AG  Search this
Materials:
steel
Dimensions:
Overall: 74 in. tall x 43 in. diameter (187.96 x 109.22cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
Germany
Credit Line:
Transferred from the U.S. Air Force
Inventory Number:
A19730005000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9e51851b9-8e9d-46b6-b3e2-545b67369769
EDAN-URL:
edanmdm:nasm_A19730005000
Online Media:

Injector, Rocket Engine, Liquid Fuel, M-1

Manufacturer:
Aerojet Electrosystems Inc.  Search this
Materials:
Copper baffles; overall, stainless steel
Dimensions:
Overall: 17 in. long x 52 in. diameter, 3658 lb. (43.18 x 132.08cm, 1659.3kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Date:
ca. 1962-1968
Credit Line:
Gift of the Aerojet General Corporation
Inventory Number:
A19700245000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9a5da239f-e187-42c4-8744-ba9f3613d244
EDAN-URL:
edanmdm:nasm_A19700245000
Online Media:

Rocket Engine, Liquid Fuel, RL-10

Manufacturer:
Pratt & Whitney  Search this
Materials:
Chamber, 347 stainless steel brazed with silver; piping, polished stainless steel; pump, aluminum casting; heat exchanger, nickel alloy
Dimensions:
Overall: 27 9/16 in. tall x 70 in. long x 40 in. diameter (70 x 177.8 x 101.6cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the NASA Marshall Space Flight Center
Inventory Number:
A19940100000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv91364251e-b0cd-4bcc-b992-7f66c3ec652d
EDAN-URL:
edanmdm:nasm_A19940100000

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:
Usage conditions apply
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
GUID:
http://n2t.net/ark:/65665/nv991252ad7-8bd0-4dc9-a031-380f39eb444c
EDAN-URL:
edanmdm:nasm_A19680012000

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