Encyclopedia Astronautica
Goddard L-B



god37van.jpg
Goddard series L sec
Rocket was equipped with gyro, air and blast vanes.
American test vehicle. The L-B series were check tests of 5.75-in.-diameter chambers with fuels of various volatilities; development of tilting cap parachute release; tests of various forms of exposed movable air vanes; test of retractable air vanes and parachute with heavy shroud lines. The series ran from November 24, 1930-May 19, 1937 (L8-L15). Final results of Section B of L Series showed two proving-stand tests, and six flight test attempts, all of which resulted in flights. Average interval between tests 22 days.

Height: 5.07 m (16.63 ft).
Diameter: 0.23 m (0.75 ft).
First Launch: 1936.12.18.
Last Launch: 1937.05.19.
Number: 6 .

More... - Chronology...


Associated Countries
See also
  • Goddard Robert H. Goddard was the father of American rocketry. In a series of rockets flown between World War I and World War II, he solved all of the fundamental problems of guided liquid propellant rockets. More...

Associated Manufacturers and Agencies

Goddard L-B Chronology


1936 November 24 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Goddard series L section B liquid rocket tests. - . Nation: USA. Related Persons: Goddard. These were check tests of 5 3/4-in.-diameter chambers with fuels of various volatilities; development of tilting cap parachute release; tests of various forms of exposed movable air vanes; test of retractable air vanes and parachute with heavy shroud lines. The series ran from November 24, 1930-May 19, 1937 (L8-L15).

1936 December 18 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 0.0010 km (0.0006 mi). Summary: Rocket was equipped with a pressure storage tank; rocket turned sharply to the right soon after it emerged from the tower, and proceeded at 150 angle above the horizontal until it landed 2000 ft from tower; noise heard at ranch house, 8 miles away..

1937 February 1 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 0.57 km (0.35 mi). Summary: Rocket was equipped with gyro, air and blast vanes; length 16 ft 7 5/8 in.; diameter 9 in.; altitude 1870 ft; duration 20.5 sec; corrected well; ground behind flame deflector turned green and glazed by heat..

1937 February 27 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 0.46 km (0.29 mi). Summary: Rocket was equipped with new parachute release operated by gyro; altitude 1500 ft; duration 20 sec; speed very high; landed 3000 ft from tower, softened ground for considerable distance..

1937 March 26 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 2.60 km (1.62 mi). Summary: Rocket was equipped with larger movable air vanes; altitude 8000-9000 ft; duration 22.3 sec; corrected while propulsion lasted, then tilted; altitude uncertain because of haze remaining from dust storms..

1937 April 22 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 2.00 km (1.20 mi). Summary: Rocket was equipped with larger movable air vanes and reinforced parachute; length 17 ft 9 in.; diameter 9 in.; duration 21.5 sec; could not be followed to top of flight, as it was nearly overhead; landed 1 mile from tower..

1937 May 19 - . LV Family: Goddard. Launch Vehicle: Goddard L-B.
  • Final flight of Goddard series L section B rocket - . Nation: USA. Related Persons: Goddard. Apogee: 0.99 km (0.62 mi). Rocket was equipped with streamline retractable air vanes and wire-wound pressure storage tank; length 17 ft 8 in.; diameter 9 in.; altitude 3250 ft; duration 29.5 sec; much-improved stabilisation. Final results of Section B of L Series, from November 1936-May 1937, showed two proving-stand tests, and six flight test attempts, all of which resulted in flights. Average interval between tests 22 days

Home - Browse - Contact
© / Conditions for Use