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1911 documents - page 1 of 96

Nozzle, Extension, for Apollo Service Module Propulsion System (SMS)

Manufacturer:
Aerojet General Corp.  Search this
Materials:
Overall, non-ferrous metal, thin gauge, probably columbium and titanium
Dimensions:
Approximate: 8ft 2 1/2in. x 9ft 4in. (250.19 x 284.48cm)
Type:
PROPULSION-Miscellaneous
Country of Origin:
United States of America
Credit Line:
Transferred from NASA/Johnson Space Center
Inventory Number:
A19780061002
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_A19780061002
Additional Online Media:

Rocket Engine, Relief Valves and Nozzles, Viking Orbiter Propulsion System

Manufacturer:
Jet Propulsion Laboratory, California Institute of Technology  Search this
Materials:
Aluminum
Dimensions:
3-D (Overall, each rod): 93 × 3cm (3 ft. 5/8 in. × 1 3/16 in.)
Type:
PROPULSION-Accessories (to an Engine)
Country of Origin:
United States of America
Credit Line:
Transferred from NASA - Jet Propulsion Laboratory
Inventory Number:
A19960003001
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_A19960003001

Injector Head, Liquid Fuel, Apollo Service Propulsion System (SPS)

Manufacturer:
Aerojet General Corp.  Search this
Materials:
Aluminum alloy
Dimensions:
Overall: 1ft 6 1/2in. x 2ft x 1ft 11in. (47 x 61 x 58.42cm)
Type:
PROPULSION-Accessories (to an Engine)
Country of Origin:
United States of America
Date:
ca. 1967
Credit Line:
Gift of Aerojet General Corp.
Inventory Number:
A19680474000
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_A19680474000

Rocket Engine, Liquid Fuel, Propulsion System, Viking Orbiter

Manufacturer:
NASA - Jet Propulsion Laboratory  Search this
Materials:
Main support ring, aluminum; tanks (3), stainless steel
Dimensions:
Height, 9 feet 2 inches; diameter, 6 feet 9.5 inches;
Weight 450 LBS.
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from NASA, Jet Propulsion Lab
Inventory Number:
A19960003000
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_A19960003000

Rocket Engine, Liquid Fuel, Ranger Midcourse Propulsion System

Materials:
Tanks, stainless steel; thrust chamber, stainless steel; vane actuators, aluminum
Dimensions:
Overall: 1 ft. 11 1/2 in. tall x 1 ft. 4 in. wide (59.7 x 40.6cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from NASA, Jet Propulsion Lab, Pasadena, Calif.
Inventory Number:
A19960004000
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_A19960004000
Additional Online Media:

Rocket Engine, Liquid, Chamber, Apollo Service Module Propulsion System (SPS)

Manufacturer:
Aerojet General Corp.  Search this
Materials:
Combustion chamber, rubberized, phenolic refrasil inner liner, an ablative or heat-resistant material. Aluminum flange bonded to inner liner. Propellant lines, 304L stainless steel. Valves, cast aluminum. Injector, Type 6061-T6 aluminum alloy. Other parts, stainless steel; fixture brackets, steel.
Aluminum, Stainless Steel, Paint, Plastic, Paper, Adhesive, Ink, Synthetic Fabric
Dimensions:
Overall: 5 ft. 3 in. tall x 4 ft. 5 in. wide, 3850 lb. (160.02 x 134.62cm, 1746.3kg)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19860252000
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:
Human Spaceflight
Data Source:
National Air and Space Museum
EDAN-URL:
edanmdm:nasm_A19860252000
Additional Online Media:

Rocket Engine, Liquid Fuel, Auxiliary Propulsion System (APS), Thruster, Saturn

Manufacturer:
TRW, Inc., Electromechanical Division  Search this
Materials:
Nozzle and chamber, phenolic impregnated silica with fiberglass overwrap; nozzle, sprayed zirconia coating; propellant inlets and valves, metal
Dimensions:
Overall: 1 ft. 7 in. long x 1 ft. 2 1/2 in. diameter (48.26 x 36.83cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Gift of McDonnell Douglas Astronautics Company
Inventory Number:
A19740781000
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_A19740781000

Rocket Engine, Liquid Fuel, Auxiliary Propulsion System (APS), Thruster, Saturn

Manufacturer:
TRW, Inc., Electromechanical Division  Search this
Materials:
Nozzle and chamber, brown phenolic impregnated silica with fiberglass overwrap; nozzle, sprayed zirconia coating; propellant inlets and valves, metal; white insulated plastic strands of wire, eight.
Dimensions:
Overall: 19 in. long x 14 1/2 in. diameter (48.26 x 36.83cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Gift of McDonnell Douglas Astronautics Company
Inventory Number:
A19740784000
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_A19740784000

Rocket Engine, Liquid Fuel, Auxiliary Propulsion System (APS), Thruster, Saturn

Manufacturer:
TRW, Inc., Electromechanical Division  Search this
Materials:
Molybdenum throat; sprayed zirconia coating on same; fiberglass covering on the main rocket motor chamber, with under coat of phenolic impregnated silica
Dimensions:
Overall: 7 in. wide x 15 in. long, 11 lb. (17.78 x 38.1cm, 5kg)
Other (Motor Chamber): 6 1/2 in. diameter (16.51cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Gift of McDonnell-Douglas Astronautics Company
Inventory Number:
A19740786000
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_A19740786000

Rocket Motor, Liquid Propellant, Minuteman Missile Post-Boost Propulsion System

Manufacturer:
Bell Aerosystems Company  Search this
Materials:
Magnesium, beryllium, paint, teflon, Aluminum, Cadmium Plating, Fiberglas, Stainless Steel, Rubber (Silicone), cork, paper, Adhesive
Dimensions:
Approximate: 133.35 x 64.77cm (4ft 4 1/2in. x 2ft 1 1/2in.)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Gift of Bell Aerospace Company
Inventory Number:
A19770994000
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_A19770994000
Additional Online Media:

Rocket Engine, Liquid, Chamber, Apollo Service Module Propulsion System (SPS)

Manufacturer:
Aerojet General Corp.  Search this
Materials:
Combustion chamber, rubberized, phenolic refrasil inner liner, an ablative, or heat-resistant material. Aluminum flange bonded to inner liner. Propellant lines, 304L stainless steel. Valves. cast aluminum. Injector, Type 6061-T6 aluminum alloy. Other parts, stainless steel; fixture brackets, steel.
Dimensions:
Overall: 3ft 6in. x 5ft 4in. (106.68 x 162.56cm)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred from NASA/Johnson Space Center
Inventory Number:
A19780061000
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_A19780061000
Additional Online Media:

Rocket Engine, Liquid Fuel, Auxiliary Propulsion System (APS), Thruster, Saturn

Manufacturer:
TRW, Inc., Electromechanical Division  Search this
Materials:
Phenolic Resin
Steel
Anodized Aluminum
Plastic
Sythetic Rubber
Adhesive
Paper
Paint
Nozzle and chamber, phenolic impregnated silica with fiberglass overwrap; nozzle, sprayed zirconia coating; propellant inlets and valves, metal.
Dimensions:
16 15/16" x 9" x 7"
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred to the National Air and Space Museum from the McDonnell Douglas Astronautics Co.
Inventory Number:
A19740782000
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_A19740782000
Additional Online Media:

Rocket Engine, Liquid Fuel, Auxiliary Propulsion,System (APS) Thruster, Saturn V

Manufacturer:
TRW, Inc., Electromechanical Division  Search this
Materials:
Anodized aluminum, steel, stainless steel, non-magnetic metal, adhesive tape, paper labels, plastic, electrical wires, micarta, rubber.
Dimensions:
29.2cm (11 1/2in.) (Approximate, tall cylinder)
19.1 x 19.7cm (7 1/2in. x 7 3/4in.) (Approximate, injector)
Type:
PROPULSION-Rocket Engines
Country of Origin:
United States of America
Credit Line:
Transferred to the National Air and Space Museum from the McDonnell Douglas Astronautics Co.
Inventory Number:
A19740780000
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_A19740780000
Additional Online Media:

Curtiss, General. [glass negative]

Photographer:
Curtiss Aeroplane and Motor Company  Search this
Type:
Glass negatives
Topic:
Propulsion systems  Search this
Local number:
NASM-CW5G-0186
Restrictions & Rights:
Images are subject to Smithsonian Institution, National Air and Space Museum, Copyright and Image Use Restrictions. Usage requires prior written permission. Should you wish to use NASM still images in any medium, please submit an Application for Permission to Reproduce NASM Photographs, available at NASM's Permissions webpage: www.nasm.si.edu/research/arch/permissions.cfm
See more items in:
Curtiss-Wright Corporation Records
Data Source:
National Air and Space Museum Archives
EDAN-URL:
edanmdm:siris_arc_384823

Propulsion, Engines, Curtiss, General. [glass negative]

Photographer:
Curtiss Aeroplane and Motor Company  Search this
Type:
Glass negatives
Topic:
Propulsion systems  Search this
Local number:
NASM-CW5G-0363
Restrictions & Rights:
Images are subject to Smithsonian Institution, National Air and Space Museum, Copyright and Image Use Restrictions. Usage requires prior written permission. Should you wish to use NASM still images in any medium, please submit an Application for Permission to Reproduce NASM Photographs, available at NASM's Permissions webpage: www.nasm.si.edu/research/arch/permissions.cfm
See more items in:
Curtiss-Wright Corporation Records
Data Source:
National Air and Space Museum Archives
EDAN-URL:
edanmdm:siris_arc_386771

Propulsion, Engines, Guiberson Diesel T-1020 9-Cylinder Radial Tank Engine. [photograph]

Photographer:
Unknown  Search this
Type:
Photographs
Topic:
Propulsion systems  Search this
Local number:
NASM-9A13696
Restrictions & Rights:
Images are subject to Smithsonian Institution, National Air and Space Museum, Copyright and Image Use Restrictions. Usage requires prior written permission. Should you wish to use NASM still images in any medium, please submit an Application for Permission to Reproduce NASM Photographs, available at NASM's Permissions webpage: www.nasm.si.edu/research/arch/permissions.cfm
See more items in:
Fred A. Thaheld Collection
Data Source:
National Air and Space Museum Archives
EDAN-URL:
edanmdm:siris_arc_388018

Whittle, Frank J.; Engines, Power Jets (Whittle) W1X Turbojet. [photograph]

Photographer:
Unknown  Search this
Type:
Photographs
Date:
Circa 1974-75
Topic:
Propulsion systems  Search this
Local number:
NASM-75-16332
Restrictions & Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use Smithsonian National Air and Space Museum (NASM) material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at http://airandspace.si.edu/permissions
See more items in:
National Air and Space Museum Cataloged Imagery Collection
Data Source:
National Air and Space Museum Archives
EDAN-URL:
edanmdm:siris_arc_364256

Schilling Canal Boat Propulsion System, Patent Model

Patentee:
Schilling, Cornelius  Search this
Inventor:
Schilling, Cornelius  Search this
Physical Description:
brass (overall material)
tin (overall material)
Measurements:
overall: 10 in x 4 in x 3 1/2 in; 25.4 cm x 10.16 cm x 8.89 cm
Object Name:
canal boat propulsion, patent model
patent model, boat propulsion, canal
Associated Place:
United States: New York
Associated place:
United States: New York, New York City
Date made:
1871
Patent date:
1871-10-10
Subject:
Patent Models  Search this
ID Number:
1979.1029.02
Catalog number:
1979.1029.02
Accession number:
1979.1029
Patent number:
119,792
See more items in:
Work and Industry: Maritime
America on the Move
Transportation
Data Source:
National Museum of American History
EDAN-URL:
edanmdm:nmah_1316598

Rocket Motor, Ion, Cesium, SERT 2

Manufacturer:
NASA, Lewis Research Center  Search this
Materials:
Stainless Steel
Plastic
Brass
Ceramic
Dimensions:
Overall (Bottom Piece): 7.9 x 12.1cm (3 1/8in. x 4 3/4in.)
Overall (Top Piece): 13.7 x 7.6cm (5 3/8in. x 3in.)
Type:
PROPULSION-Miscellaneous
Country of Origin:
United States of America
Credit Line:
Transferred from NASA Marshall Spaceflight Center
Inventory Number:
A19760724000
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_A19760724000
Additional Online Media:

Boeing Model 367-80 (707 Prototype). [photograph]

Photographer:
Unknown  Search this
Type:
Photographs
Topic:
Aeronautics  Search this
Airplanes  Search this
Propulsion systems  Search this
Local number:
NASM-14618
Restrictions & Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use Smithsonian National Air and Space Museum (NASM) material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at http://airandspace.si.edu/permissions
See more items in:
Videodisc Imagery Collection
Data Source:
National Air and Space Museum Archives
EDAN-URL:
edanmdm:siris_arc_364011

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