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Goddard 4
Part of Goddard
American test vehicle. Goddard rocket using pressure-fed LOx/Gasoline propellants, streamline casing, and remote control guidance. Masses varied; typical values indicated.
 Status: Retired 1931.  First Launch: 1930-12-30.  Last Launch: 1931-10-27.  Number:  4 . Payload: 1.00 kg (2.20 lb). Gross mass: 40 kg (88 lb). Height: 3.00 m (9.80 ft). Diameter: 0.30 m (0.98 ft). Apogee: 610 km (370 mi). 
Payload: 1.00 kg (2.20 lb) to a 610 m altitude.
Family: 
Early Rocketry, 
test vehicle. 
People: 
Goddard. 
Country: 
USA. 
1929 December 3 - 1930 June 30 - . 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard rockets tests at Camp Devens - . 
Nation: USA. 
Related Persons: Goddard. 
Goddard conducts tests at the artillery range at Camp Devens, 25 miles from Worcester, for the improvement of liquid-fuel rocket-motor efficiency, particularly the 'curtain cooling.' Sixteen proving-stand tests were made; there were no flight tests. A few special tests were made with rocket-operated propellers. 
1930 July - . 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard moves rocket work to Roswell, New Mexico - . 
Nation: USA. 
Related Persons: Goddard. 
Goddard's liquid rocket development project was moved to New Mexico under the auspices of Daniel Guggenheim of New York City. Dr. Goddard could now devote full time to the rocket work. . 
1930 October 23 - . 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
1930 December 30 - . 
Launch Site: 
Auburn. 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard's fifth flight of a liquid fuel rocket - . 
Nation: USA. 
Related Persons: Goddard. 
Apogee: 0.61 km (0.38 mi). The rocket reached an altitude of 2000 ft and a maximum speed of 500 mph. The vehicle was 11 ft long; empty weight 33.5 lb; a gas pressure tank was used to force liquid oxygen and gasoline into combustion chamber.. 
1931 September 29 - . 
Launch Site: 
Roswell. 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard rocket flight test - . 
Nation: USA. 
Related Persons: Goddard. 
Apogee: 0.0550 km (0.0342 mi). Flight of Goddard liquid fuel rocket with jacket, streamline casing, remote control. Length, 9 ft 11 in.; diameter 12 in.; weight empty 37 lb; weight loaded 87.2 lb; in air 9.6 sec; height 180 ft; trajectory 'like a fish swimming upward.'. 
1931 October 13 - . 
Launch Site: 
Roswell. 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard rocket flight test - . 
Nation: USA. 
Related Persons: Goddard. 
Apogee: 0.52 km (0.32 mi). Flight of Goddard liquid fuel rocket with simplified combustion chamber, parachute releasing. Length 7 ft 9 in.; diameter 12 in.; height 1700+ ft; loud whistling on descent.. 
1931 October 27 - . 
Launch Site: 
Roswell. 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard rocket flight test - . 
Nation: USA. 
Related Persons: Goddard. 
Apogee: 0.41 km (0.25 mi). Range: 0.28 km (0.18 mi). Flight of Goddard liquid fuel rocket with new gasoline shutoff valve. Dimensions similar to October 13; altitude 1330 ft; landed 930 ft from tower; in air 8.6 sec.. 
1931 November 23 - . 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard rocket static test - . 
Nation: USA. 
Related Persons: Goddard. 
Static test of Goddard liquid fuel rocket with modified oxygen injection; lift 270 lb for 11 sec; jet velocity 5088 ft/sec. . 
1932 April 19 - . 
LV Family: 
Goddard. 
Launch Vehicle: 
Goddard 4. 
- Goddard tests rocket with gyro stabilization. - . 
Nation: USA. 
Related Persons: Goddard. 
Apogee: 0.0410 km (0.0255 mi). Flight of Goddard liquid fuel rocket with pressure generated by liquid nitrogen, and eight gyro-controlled vanes (four into blast and four into slipstream) for stabilisation. Length 10 ft 9.5 in.; weight empty 19.5 lb; height 135 ft; in air 5 sec.. 
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