example.json

{
    "name": "Rocket Equation",
    "latex": "$$\\Delta v = I_{sp} \\, g_0 \\, \\ln \\left( \\frac{m_0}{m_f} \\right)$$",
    "description": "The Tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation is a mathematical equation that describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity can thereby move due to the conservation of momentum.",
"definition":{
    "\\Delta V" : "change in velocity (m/s)",
    "I_{sp} " : "specific impulse (s)",
    "m_0" : "initial mass (kg)",
    "m_f" : "final mass (kg)"
},
    "keywords": ["rocket", "delta-v", "tsiolkovski", "momentum", "propulsion"],
    "tags": ["Aerospace", "default"],
    "href": "https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation",
    "contributed_by": "Hannibal Lecter"
}