Status: Retired 1999. First Launch: 1976-07-22. Last Launch: 1999-07-01. Number: 4 . Thrust: 57.00 kN (12,814 lbf). Gross mass: 100 kg (220 lb). Height: 2.40 m (7.80 ft). Diameter: 0.41 m (1.34 ft). Apogee: 165 km (102 mi).
|Nike Malemute American sounding rocket. Two stage vehicle consisting of 1 x Nike + 1 x Malemute|
|Terrier Malemute American sounding rocket. The Terrier-Malemute launch vehicle was a high performance two-stage vehicle used for payloads weighing less than 180 kg, generally used for relatively lightweight plasma physics payloads. Payload 90 kg to 650 km or 180 kg to 420 km.|
|1.5KS35000 Thiokol solid rocket engine.|
|Terrier Improved Malemute American sounding rocket. Version with higher performance version of Malemute second stage.|
|Imp. Malemute Single stage sounding rocket using improved Malemute motor.|