JB-3 Tiamat
id:
jb-3-tiamat-173-14081158
title:
JB-3 Tiamat
text:
The JB-3 Tiamat was subsonic air-to-air missile program that began in January 1944 for the U.S. Army Air Force under project MX-570. The prime contractor was Hughes Aircraft Company Electronics Division which developed the Tiamat with the assistance of the National Advisory Committee for Aeronautics (NACA). Tiamat was propelled by a rocket motor of a boost-sustain dual-thrust type, providing 7,200 lbf (32 kN) of thrust for 3.5 seconds, followed by 200 lbf (0.89 kN) for 45 seconds of cruising fli
brand slug:
wiki
category slug:
encyclopedia
description:
Air-to-air missile
original url:
https://en.wikipedia.org/wiki/JB-3_Tiamat
date created:
2017-12-17T06:51:18Z
date modified:
2024-09-02T22:10:23Z
main entity:
{"identifier":"Q48977185","url":"https://www.wikidata.org/entity/Q48977185"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/6/68/JB-3_Tiamat.jpg","width":601,"height":312}
fields total:
13
integrity:
16