Rockets, Missiles, and Spacecraft of the National Air and Space Museum, Smithsonian InstitutionMurphy, Lynne C.
History
Rockets, Missiles, and Spacecraft of the National Air and Space Museum, Smithsonian Institution
Murphy, Lynne C.
Astronautics -- United States -- Exhibitions; National Air and Space Museum
Height 3 m. (10 ft.)
Distance across 3.5 m. (11 ft., 6 in.)
footpads
Weight 1000 kg. (2204 lb.) at launch; 292 kg. (644 lb.)
as exhibited
Electrical power One .83 sq. m. (9 sq. ft.) solar panel providing
89 w. to a silver-zinc battery
Landing vernier Three throttleable liquid-propellant rockets
rocket system each providing from 14.6 to 47.2 kg. thrust
(30 to 104 lb. thrust).
Fuel—Monomethylhydrazine monohydrate; oxidizer
90% nitrogen tetroxide and 10% nitric oxide.
Goddard Rockets: May 1926 and “Hoopskirt,” 1928
The American pioneer of astronautics, Robert H. Goddard (1882-1945) not
only outlined the physical principles that would govern space flight,
but he also constructed and tested many rocket engines, airframes,
control devices, and guidance mechanisms between 1926 and 1942.
Goddard held a doctorate in physics, and was a professor at Clark
University, Worcester, Massachusetts. The Smithsonian Institution began
funding Goddard’s experiments as early as 1917 and published his first
major work, _A Method of Reaching Extreme Altitudes_, in 1919.
Goddard was not only a trained scientist, but a talented and ingenious
engineer as well. On March 16, 1926, he launched the world’s first
liquid-propellant rocket. By 1930, he had established a rocket test
facility at Mescalero Ranch, near Roswell, New Mexico. Here, he
conducted research, funded by the Daniel and Florence Guggenheim
Foundation, on rocket power plants, pumps and fuel systems, control
mechanisms, and other vital elements of the modern rocket.
The Rocket of May 4, 1926
This vehicle is the oldest surviving liquid-propellant rocket in the
world. Built of parts employed in the first liquid-propellant rocket
launched on March 16, 1926, the engine was moved from the nose of the
vehicle to the rear for the May 4 trial. Other changes were introduced
to reduce the weight of the rocket to 2.5 kilograms (5.5 pounds). The
motor burned gasoline and liquid oxygen.
The alcohol burner under the liquid oxygen tank was inadvertently not
ignited, causing the May 4 attempted launch to fail. A second test on
May 5 also proved unsuccessful. However, the rocket engine was fired on
both occasions.
The May 4 rocket is from Mrs. Robert H. Goddard and the Daniel and
Florence Guggenheim Foundation.
May 1926 rocket
Length 1.95 m. (6 ft., 4 in.)
Weight 2.5 kg. (5.5 lb.)
Fuel Gasoline
Oxidizer Liquid oxygen
The “Hoopskirt” Rocket
[Illustration: 45. Dr. Goddard and the “Hoopskirt.” Propellant tanks
are on legs of frame.]
[Illustration: 46. The upper section of the “Hoopskirt” rocket.]
Public-domain text, read in full here on John Shaqi.
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