KDU-414

Summary

KDU-414 is an engine model^[1]. KDU-414 draws 8 Wikipedia views per month (engine_model category, ranking #183 of 519).^[2]

Key Facts

• KDU-414's image is recorded as Russian thruster2.jpg^[3].
• KDU-414's instance of is recorded as engine model^[4].
• KDU-414's manufacturer is recorded as A.M. Isayev Chemical Engineering Design Bureau^[5].
• KDU-414's subclass of is recorded as liquid propellant rocket engine^[6].
• KDU-414's subclass of is recorded as pressure-fed engine^[7].
• KDU-414's designed by is recorded as Aleksey Isayev^[8].
• KDU-414's Commons category is recorded as KDU-414^[9].
• KDU-414's country of origin is recorded as Soviet Union^[10].
• KDU-414's first flight is recorded as +1960-00-00T00:00:00Z^[11].
• KDU-414's source of energy is recorded as mélange^[12].
• KDU-414's source of energy is recorded as 1,1-dimethylhydrazine^[13].
• KDU-414's service retirement is recorded as +1974-00-00T00:00:00Z^[14].
• KDU-414's GRAU index is recorded as 11Д414^[15].
• KDU-414's length is recorded as {'unit': 'Q11573', 'amount': '+1.02'}^[16].
• KDU-414's mass is recorded as {'unit': 'Q11570', 'amount': '+61'}^[17].
• KDU-414's maximum thrust is recorded as {'unit': 'Q56402798', 'amount': '+1.96'}^[18].
• KDU-414's diameter is recorded as {'unit': 'Q11573', 'amount': '+0.74'}^[19].
• KDU-414's Google Knowledge Graph ID is recorded as /g/121gjy5q^[20].
• KDU-414's specific impulse by weight is recorded as {'unit': 'Q11574', 'amount': '+272'}^[21].

Body

Physical Characteristics

KDU-414's length is recorded as {'unit': 'Q11573', 'amount': '+1.02'}^[16].

Designation and Status

KDU-414's instance of is recorded as engine model^[4].

Why It Matters

KDU-414 draws 8 Wikipedia views per month (engine_model category, ranking #183 of 519).^[2] KDU-414 has Wikipedia articles in 7 language editions, a strong signal of global cultural recognition.^[22] KDU-414 is known by 3 alternative names across languages and contexts.^[23]