AKA: AIM-7;Hydra-Iris-0. Status: Retired 1968. Gross mass: 100 kg (220 lb). Height: 1.60 m (5.20 ft). Diameter: 0.41 m (1.34 ft).
Naval Prop Plant solid rocket engine. Hydra-Iris zero stage.
Subtopics MARC 14B1 ARC solid rocket engine. Cluster of Sparrow motors. 1.8KS7800 Multiple-source American solid rocket engine. Sparoair II first stage. Country: USA. Launch Vehicles: Hydra-Iris. Propellants: Solid. Stages: Sparrow. Agency: USN, USN Naval Prop Plant. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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