TEPREL-B

Summary

TEPREL-B is an engine model^[1].

Key Facts

• TEPREL-B's image is recorded as Motor TEPREL-C durante el lanzamiento exitoso del cohete MIURA 1 (cropped).jpg^[2].
• TEPREL-B's instance of is recorded as engine model^[3].
• TEPREL-B's manufacturer is recorded as PLD Space^[4].
• TEPREL-B's developer is recorded as PLD Space^[5].
• TEPREL-B's subclass of is recorded as liquid propellant rocket engine^[6].
• TEPREL-B's subclass of is recorded as pressure-fed engine^[7].
• TEPREL-B's part of is recorded as TEPREL^[8].
• TEPREL-B's country of origin is recorded as Spain^[9].
• TEPREL-B's first flight is recorded as +2023-10-07T00:00:00Z^[10].
• TEPREL-B's source of energy is recorded as kerolox^[11].
• TEPREL-B's used by is recorded as Miura 1^[12].
• TEPREL-B's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+30'}^[13].

Body

Geography

TEPREL-B's part of is recorded as TEPREL^[8].

Designation and Status

TEPREL-B's instance of is recorded as engine model^[3].