Reference · Rockets, variants, parts and the fit check
PROPELLANTSconstant
The engines whose propellant a page read here names. Each propellant is a figure with its page; the flame kind follows from it (a test holds the two together).
Import it
import { PROPELLANTS } from "@johnmorrisdotca/uchusen-rockets";Definition
const PROPELLANTS: readonly EnginePropellant[]Examples
import { PROPELLANTS } from "@johnmorrisdotca/uchusen-rockets";
console.log(PROPELLANTS.map((one) => `${one.name}: ${one.propellant.value}`));[
'Merlin: LOX / RP-1',
'Kestrel: LOX / RP-1',
'Raptor: LOX / CH4',
'F-1: LOX / RP-1',
'J-2: Liquid oxygen / Liquid hydrogen',
'RS-25: LOX / LH2',
'Space Shuttle solid rocket booster: Ammonium perchlorate, aluminium powder and PBAN (APCP)',
'SLS solid rocket booster: PBAN-APCP',
'BE-4: LOX / CH4',
'BE-3: LOX / LH2',
'Rutherford: LOX / RP-1',
'RD-107 and RD-108: LOX / RG-1',
'Lunar module descent engine: Aerozine 50 fuel / nitrogen tetroxide oxidizer'
]What it prints (run when this page was built)