Tsiolkovsky delta-v

Frammenti di codice

curl "https://api.oanor.com/rocket-api/v1/delta-v" \
  -H "x-oanor-key: oanor_test_..."

await fetch("https://api.oanor.com/rocket-api/v1/delta-v", {
  headers: { "x-oanor-key": "oanor_test_..." }
});

$ch = curl_init("https://api.oanor.com/rocket-api/v1/delta-v");
curl_setopt($ch, CURLOPT_HTTPHEADER, ["x-oanor-key: oanor_test_..."]);
curl_setopt($ch, CURLOPT_RETURNTRANSFER, true);
$out = curl_exec($ch);

import requests
requests.get(
    "https://api.oanor.com/rocket-api/v1/delta-v",
    headers={"x-oanor-key": "oanor_test_..."}
)

Risposta di esempio

Una risposta reale di questo endpoint, acquisita dall'ultimo health check.

{
    "data": {
        "note": "Tsiolkovsky rocket equation Δv = ve·ln(m0/mf), with exhaust velocity ve = Isp·g0. The Δv budget determines what manoeuvres a stage can perform.",
        "inputs": {
            "dry_mass": 400,
            "wet_mass": 1000,
            "exhaust_velocity_ms": 2941.995
        },
        "delta_v_ms": 2695.7228,
        "mass_ratio": 2.5,
        "delta_v_kms": 2.695723,
        "propellant_mass": 600
    },
    "meta": {
        "timestamp": "2026-06-05T11:30:29.002Z",
        "request_id": "58686881-d5a9-4a92-a24a-464976b13b9d"
    },
    "status": "ok",
    "message": "Delta-v",
    "success": true
}