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Background | Achievements | Timeline | Pictures | Bibliography |
Timeline of Robert Goddard's Life 1,5
1882, October 5th Born at Maple Hill, Worcester, MA
1889 At age 7, began thinking about flight into outer space
1904-1908 Student, Worcester Polytechnic Institute (B.S. 1908)
1908-1909 Instructor of Physics, W.P.I., & special student in Physics, Clark University
1909-1911 Fellow in Physics, Clark University (A.M. 1910, Ph.D. 1911)
1911-1912,
1914-1915, Honorary Fellow in Physics, Clark University
1918-1920
1912 First explored mathematically the practicality of
using rocket power to reach high altitudes &
escape velocity
1912-1913 Research Instructor in Physics, Princeton University
1913-1914 Illness--tuberculosis
1914, July Awarded first two patents for his liquid-fuel gun
rocket and a multistage step rocket rocket1914-1915 Instructor, Clark College
1915 Proved experimentally that a rocket will provide thrust in a vacuum
1915-1919 Assistant Professor, Clark College1917-1918 Developed the basis for the rocket weapon, later
known as the bazooka, for the U.S. Army
1919 First to publish in the U.S. a basic mathematical
theory underlying rocket propulsion & rocket
flight, together with results of experiments
with solid-propellant rockets. It was titled "A Method of
Reaching Extreme Altitudes"1919-1920 Associate Professor, Clark College
1920-1923 Part-time consultant on solid-propellant rocket
weapons for U.S. Government at Indian Head,
Maryland
1920-1925 Developed the first rocket motor using liquid propellants (liquid oxygen & gasoline)
1920-1943 Professor, Clark University
1923-1943 Director of the Physical Laboratories, Clark University
1924, June 21 Married Esther Christine Kisk
1925 Static test at Clark University: liquid-propellant rocket
lifted its own weight for the first time
1926, March 16 First launch of a liquid-propellant rocket, at Auburn, MA
1929, July 17 Tested first rocket containing instruments
1929, November 23 First met with Charles A. Lindbergh, who was later influential in helping
Goddard receive funding for his work
1930-1932 Began conducting full time rocket research at Roswell, NM on leave
of absence from Clark University
1932 Developed first gyro stabilization apparatus for rockets
1932 First used deflector vanes in the blast of the rocket motor as
a method of stabilizing & guiding rockets
1932-1934 Continued teaching at Clark University while also carrying on his research
1935 Conducted a series of 14 tests with rockets that were about 15 feet long
1935, March 8 Launched the first liquid-propellant rocket which attained a speed greater
than that of sound (700 mph)
1935 Rocket reached altitude of 7500 feet
1936, March 16 Published "Liquid Propellant Rocket Development"
1936-1938 Conducted a series of 30 tests with rockets that were about 18 feet long
1937, March 26 Rocket reached height of 9000 feet; his highest flight
1938-1941 Conducted a series of 36 tests with rockets that were about 22 feet long;
these were his last flight tests
1942-1945 Worked as Director of Research for the Navy Department, Bureau
of Aeronautics developing jet-assisted takeoff and variable-thrust
liquid-propellant rockets
1943-1945 Worked as a Consulting Engineer for Curtiss-Wright Corporation
1944-1945 Was the director of the American Rocket Society
1945, June 2 Received an honorary Doctor of Science degree from Clark University
1945, August 10 Died at Baltimore, MD. Buried in Hope Cemetery, Worcester, MA