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HJ Nike Gosling
Part of Honest John
American test vehicle. Three stage vehicle consisting of 1 x M-6 + 1 x Nike + 1 x Gosling
Status: Retired 1960. First Launch: 1960-04-26. Last Launch: 1960-10-19. Number: 3 . Thrust: 365.00 kN (82,055 lbf). Height: 10.00 m (32.00 ft). Diameter: 0.58 m (1.90 ft). Apogee: 20 km (12 mi).
Four Gosling motors with canted nozzles were used as boosters for the British Thunderbird ramjet surface-to-air missile. 664 Gosling IV motors were supplied for the Thunderbird, Bloodhound, and Seaslug Mark II missiles.
For sounding rocket applications, motors were supplied with in-line nozzles. The Gosling IV had an a all up mass of 256 kg, was 3.00 m long, and 0.254 m in diameter. It produced an average thrust of 124 kN over its 3.15 second burn time.
Family:
test vehicle.
Country:
USA.
Launch Sites:
Wallops Island.
Stages:
M-6,
Gosling,
M5E1.
Agency:
NASA Langley.
1960 April 26 - .
Launch Site:
Wallops Island.
LV Family:
Honest John.
Launch Vehicle:
HJ Nike Gosling.
FAILURE: Failure.
- Porous re-entry vehicle test flight - .
Nation: USA.
Agency: NASA.
Apogee: 43 km (26 mi).
1960 October 1 - .
Launch Site:
Wallops Island.
LV Family:
Honest John.
Launch Vehicle:
HJ Nike Gosling.
- E48 Re-entry vehicle Stability test - .
Nation: USA.
Agency: NASA.
Apogee: 10 km (6 mi).
1960 October 19 - .
Launch Site:
Wallops Island.
LV Family:
Honest John.
Launch Vehicle:
HJ Nike Gosling.
- E48 Re-entry vehicle Stability test - .
Nation: USA.
Agency: NASA.
Apogee: 10 km (6 mi).
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