Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage Conditions May Apply Usage Conditions Apply There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page. IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu View Manifest View in Mirador Viewer Usage conditions may apply Usage conditions may apply Usage conditions may apply

This is probably the liquid-fuel rocket Robert H. Goddard tried to launch on September 23, 1935, at Roswell, New Mexico, in an attempt to demonstrate its capabilities to supporters Charles Lindbergh and Harry Guggenheim. The Guggenheim Foundation for the Promotion of Aeronautics funded Goddard's experiments in New Mexico.

A technical problem prevented the flight. But because earlier A-series rocket launches had succeeded, Lindbergh and Guggenheim felt Goddard was on the right track. Lindbergh thus persuaded Goddard to donate a complete A-series rocket to the Smithsonian, which he did in November 1935. This rocket became the first liquid-fuel rocket in the Smithsonian collections.

Display Status

This object is not on display at the National Air and Space Museum. It is either on loan or in storage.

Object Details
Date 1935 Country of Origin United States of America Type CRAFT-Missiles & Rockets Manufacturer Dr. Robert H. Goddard
Dimensions Overall: 15 ft. 4 1/2 in. × 1 ft. × 9 in. × 1 ft. 9 1/2 in., 38.6kg (468.6 × 30.5 × 22.9 × 54.6cm, 85lb.)
Materials Aluminum skin, thin gauge, along tail section from bottom of fins to bottom of mid-section. Aluminum skin also on parachute section and nosecone wholly of spun aluminum except for steel attachment screw. Steel skin (for greater strength and insulation) below nosecone, over mid-section (over propellant tanks), and around small section above fins. One steel tube or pipe on each side of rocket, along propellant section; one smaller diameter copper tube on one side. Steel nozzle and other interior components. Fabric parachute
Alternate Name Goddard 1935 A-Series Rocket Inventory Number A19360022000 Credit Line Donated by Dr. Robert H. Goddard Data Source National Air and Space Museum Restrictions & Rights Usage conditions apply
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