_ registry / mcp http-sse · checked 57m ago

ThrustLab

https://thrustlab.com

Registry code: 0e77ecdc9807573d

api record

ThrustLab simulates electric UAV powertrains: battery, ESC, motor and propeller solved together. Use it to size a drone or aircraft powertrain and to look up real motor, propeller and battery data.

Two propeller models. The **Fast model** runs from the size printed on the propeller and answers in milliseconds; it is what these tools run. The **Full model** runs from measured blade geometry and needs a ThrustLab account. Every result says which model produced it — quote that name with the number.

endpoint
https://thrustlab.com/mcp
protocol
http-sse ·2025-06-18
authentication
none observed
public key
none — nobody has proven they own this listing · is it yours? claim it
karma
0 · newcomer
reachable
live
uptime, 30 days
100%

90 days 100%· all time 100%

latency
112ms

last good check

priced tools
0

of 7 tools

_ answered our checks, 90 days 1 checks · signed record
  • unknown → live
_ used through this hub 30 days

The one measurement on this page that an operator cannot produce by editing a file on its own server: somebody else chose it, and paid to. Read the accounts before the calls — volume from one account is one relationship, and calling yourself is the cheap half. Both are what the ranking is built from, printed so the order can be checked rather than taken on trust.

accounts
0

distinct, expensive to fake

calls served
0

successful, last 30 days

_ what it can do 7 tools
2 open 5 never probed 2 of 7 classified

Price is per tool, not per server. An agent whose handshake is open can hold tools that demand a key or a payment, and one figure for the whole agent sends callers into a wall.

  • get_validation_summary open 57m ago

    How accurate a model is, measured against wind-tunnel and bench data. `model` is "fast", "full", or an exact report slug such as "prom-5.3". The numbers are error against measured data by partition and channel, with the envelope they were measured inside. Quote the model name with the number.

    mcp-tool

    {
  "type": "object",
  "title": "get_validation_summaryArguments",
  "properties": {
    "model": {
      "type": "string",
      "title": "Model",
      "default": "full"
    }
  }
}
    arguments 11 lines
  • get_result open 57m ago

    Read a stored result: a share `token` from a run, or a `simulation_id`. `simulation_id` needs a ThrustLab API key in `Authorization: Bearer` and reads only that account's own runs.

    mcp-tool

    {
  "type": "object",
  "title": "get_resultArguments",
  "properties": {
    "token": {
      "anyOf": [
        {
          "type": "string"
        },
        {
          "type": "null"
        }
      ],
      "title": "Token",
      "default": null
    },
    "simulation_id": {
      "anyOf": [
        {
          "type": "string"
        },
        {
          "type": "null"
        }
      ],
      "title": "Simulation Id",
      "default": null
    }
  }
}
    arguments 30 lines
  • search_components unknown never probed

    Find motors, propellers or batteries in the ThrustLab database. `component_type` is "motor", "propeller" or "battery". `query` is a case-insensitive substring of the part name or its maker ("APC", "T-Motor", "13x6.5"). The maker sits under `spec.brand` for motors and batteries and under `spec.type` for propellers. `limit` is capped at 200 rows a page; when `has_more` is true, pass the returned `next_offset` as `offset` to read the next page. Each row carries its datasheet values, its source and the CC BY 4.0 attribution line. Pass a returned `id` to `simulate_powertrain`.

    mcp-tool

    {
  "type": "object",
  "title": "search_componentsArguments",
  "required": [
    "component_type"
  ],
  "properties": {
    "limit": {
      "type": "integer",
      "title": "Limit",
      "default": 25
    },
    "query": {
      "anyOf": [
        {
          "type": "string"
        },
        {
          "type": "null"
        }
      ],
      "title": "Query",
      "default": null
    },
    "offset": {
      "type": "integer",
      "title": "Offset",
      "default": 0
    },
    "sort_by": {
      "type": "string",
      "title": "Sort By",
      "default": "name"
    },
    "sort_order": {
      "type": "string",
      "title": "Sort Order",
      "default": "asc"
    },
    "component_type": {
      "type": "string",
      "title": "Component Type"
    }
  }
}
    arguments 45 lines
  • get_component unknown never probed

    Read one database row by its id (`comp_…`), with provenance. Propeller rows give diameter, pitch, blade count, weight and maximum rpm. Blade station geometry is never returned.

    mcp-tool

    {
  "type": "object",
  "title": "get_componentArguments",
  "required": [
    "component_id"
  ],
  "properties": {
    "component_id": {
      "type": "string",
      "title": "Component Id"
    }
  }
}
    arguments 13 lines
  • simulate_powertrain unknown never probed

    Solve one operating point of a whole powertrain on the Fast model. Battery, ESC, motor and propeller are solved together, so the answer is a real thrust and current, not a propeller curve. The numbers come back in `result` (`result.All` = system totals in SI units: thrust N, current A, power W, time s; one entry per rotor; `result.Battery`), with a share URL. No second call is needed to read them.

    mcp-tool

    {
  "type": "object",
  "$defs": {
    "PropellerLabel": {
      "type": "object",
      "title": "PropellerLabel",
      "required": [
        "diameter_in",
        "pitch_in"
      ],
      "properties": {
        "family": {
          "anyOf": [
            {
              "type": "string"
            },
            {
              "type": "null"
            }
          ],
          "title": "Family",
          "default": null,
          "description": "Chord-ratio preset: 'thin electric' (0.065 D), 'sport' (0.07 D), 'slow flyer' (0.10 D) or 'multirotor' (0.11 D). Defaults to sport."
        },
        "pitch_in": {
          "type": "number",
          "title": "Pitch In",
          "maximum": 400,
          "description": "Pitch in inches, e.g. 5 for a 10x5.",
          "exclusiveMinimum": 0
        },
        "camber_pct": {
          "anyOf": [
            {
              "type": "number",
              "maximum": 8,
              "minimum": 0
            },
            {
              "type": "null"
            }
          ],
          "title": "Camber Pct",
          "default": null,
          "description": "Section camber in percent. Defaults to 3.2."
        },
        "num_blades": {
          "type": "integer",
          "title": "Num Blades",
          "default": 2,
          "maximum": 8,
          "minimum": 2,
          "description": "Blade count."
        },
        "chord_ratio": {
          "anyOf": [
            {
              "type": "number",
              "maximum": 0.5,
              "exclusiveMinimum": 0
            },
            {
              "type": "null"
            }
          ],
          "title": "Chord Ratio",
          "default": null,
          "description": "Chord at 75 % radius over diameter. Give it instead of 'family' (or with family='custom'); the two cannot both be set."
        },
        "diameter_in": {
          "type": "number",
          "title": "Diameter In",
          "maximum": 400,
          "description": "Diameter in inches, e.g. 10 for a 10x5.",
          "exclusiveMinimum": 0
        }
      },
      "description": "What is printed on the propeller — all the Fast model reads.\n\nInches and a spoken family name, because that is how a propeller is sold and\nhow a user will say it. :func:`to_schema_label` turns this into the metres\nand the enum ``app.schemas.simulation.PropellerLabel`` declares."
    },
    "PowertrainInput": {
      "type": "object",
      "title": "PowertrainInput",
      "required": [
        "motor_id",
        "battery_id"
      ],
      "properties": {
        "motor_id": {
          "type": "string",
          "title": "Motor Id",
          "description": "Catalog motor public id, e.g. comp_2xK…."
        },
        "altitude_m": {
          "type": "number",
          "title": "Altitude M",
          "default": 0,
          "maximum": 11000,
          "minimum": 0
        },
        "battery_id": {
          "type": "string",
          "title": "Battery Id",
          "description": "Catalog battery public id."
        },
        "rotor_count": {
          "type": "integer",
          "title": "Rotor Count",
          "default": 1,
          "maximum": 16,
          "minimum": 1,
          "description": "Rotors on the craft."
        },
        "airspeed_m_s": {
          "type": "number",
          "title": "Airspeed M S",
          "default": 0,
          "maximum": 300,
          "minimum": 0,
          "description": "0 is a static run."
        },
        "propeller_id": {
          "anyOf": [
            {
              "type": "string"
            },
            {
              "type": "null"
            }
          ],
          "title": "Propeller Id",
          "default": null,
          "description": "Catalog propeller public id."
        },
        "throttle_pct": {
          "type": "number",
          "title": "Throttle Pct",
          "default": 100,
          "maximum": 100,
          "exclusiveMinimum": 0
        },
        "propeller_label": {
          "anyOf": [
            {
              "$ref": "#/$defs/PropellerLabel"
            },
            {
              "type": "null"
            }
          ],
          "default": null,
          "description": "Use instead of propeller_id to run from the printed size."
        }
      },
      "description": "One powertrain, as the anonymous endpoint accepts it (spec D4).\n\nCatalog components are referenced by their public id (``comp_…``, from\n``search_components``). The propeller may instead be given as a label, which\nis all the Fast model needs."
    }
  },
  "title": "simulate_powertrainArguments",
  "required": [
    "powertrain"
  ],
  "properties": {
    "powertrain": {
      "$ref": "#/$defs/PowertrainInput"
    }
  }
}
    arguments 166 lines
  • sweep_powertrain unknown never probed

    Solve a powertrain across a throttle or airspeed range, up to 25 points. `sweep.steps` is the NUMBER OF POINTS, not a step size: start 40, stop 100, steps 4 gives 40, 60, 80 and 100. One sweep beats a loop of single points. The points come back in `result.points` with the share URL; no second call is needed to read them.

    mcp-tool

    {
  "type": "object",
  "$defs": {
    "SweepAxis": {
      "type": "object",
      "title": "SweepAxis",
      "required": [
        "parameter",
        "start",
        "stop",
        "steps"
      ],
      "properties": {
        "stop": {
          "type": "number",
          "title": "Stop"
        },
        "start": {
          "type": "number",
          "title": "Start"
        },
        "steps": {
          "type": "integer",
          "title": "Steps",
          "maximum": 25,
          "minimum": 2,
          "description": "Point count, at most 25 anonymous."
        },
        "parameter": {
          "type": "string",
          "title": "Parameter",
          "description": "'throttle_pct' or 'airspeed_m_s'."
        }
      },
      "description": "A 1-D sweep axis. ``steps`` is the NUMBER OF POINTS, not a step size."
    },
    "PropellerLabel": {
      "type": "object",
      "title": "PropellerLabel",
      "required": [
        "diameter_in",
        "pitch_in"
      ],
      "properties": {
        "family": {
          "anyOf": [
            {
              "type": "string"
            },
            {
              "type": "null"
            }
          ],
          "title": "Family",
          "default": null,
          "description": "Chord-ratio preset: 'thin electric' (0.065 D), 'sport' (0.07 D), 'slow flyer' (0.10 D) or 'multirotor' (0.11 D). Defaults to sport."
        },
        "pitch_in": {
          "type": "number",
          "title": "Pitch In",
          "maximum": 400,
          "description": "Pitch in inches, e.g. 5 for a 10x5.",
          "exclusiveMinimum": 0
        },
        "camber_pct": {
          "anyOf": [
            {
              "type": "number",
              "maximum": 8,
              "minimum": 0
            },
            {
              "type": "null"
            }
          ],
          "title": "Camber Pct",
          "default": null,
          "description": "Section camber in percent. Defaults to 3.2."
        },
        "num_blades": {
          "type": "integer",
          "title": "Num Blades",
          "default": 2,
          "maximum": 8,
          "minimum": 2,
          "description": "Blade count."
        },
        "chord_ratio": {
          "anyOf": [
            {
              "type": "number",
              "maximum": 0.5,
              "exclusiveMinimum": 0
            },
            {
              "type": "null"
            }
          ],
          "title": "Chord Ratio",
          "default": null,
          "description": "Chord at 75 % radius over diameter. Give it instead of 'family' (or with family='custom'); the two cannot both be set."
        },
        "diameter_in": {
          "type": "number",
          "title": "Diameter In",
          "maximum": 400,
          "description": "Diameter in inches, e.g. 10 for a 10x5.",
          "exclusiveMinimum": 0
        }
      },
      "description": "What is printed on the propeller — all the Fast model reads.\n\nInches and a spoken family name, because that is how a propeller is sold and\nhow a user will say it. :func:`to_schema_label` turns this into the metres\nand the enum ``app.schemas.simulation.PropellerLabel`` declares."
    },
    "PowertrainInput": {
      "type": "object",
      "title": "PowertrainInput",
      "required": [
        "motor_id",
        "battery_id"
      ],
      "properties": {
        "motor_id": {
          "type": "string",
          "title": "Motor Id",
          "description": "Catalog motor public id, e.g. comp_2xK…."
        },
        "altitude_m": {
          "type": "number",
          "title": "Altitude M",
          "default": 0,
          "maximum": 11000,
          "minimum": 0
        },
        "battery_id": {
          "type": "string",
          "title": "Battery Id",
          "description": "Catalog battery public id."
        },
        "rotor_count": {
          "type": "integer",
          "title": "Rotor Count",
          "default": 1,
          "maximum": 16,
          "minimum": 1,
          "description": "Rotors on the craft."
        },
        "airspeed_m_s": {
          "type": "number",
          "title": "Airspeed M S",
          "default": 0,
          "maximum": 300,
          "minimum": 0,
          "description": "0 is a static run."
        },
        "propeller_id": {
          "anyOf": [
            {
              "type": "string"
            },
            {
              "type": "null"
            }
          ],
          "title": "Propeller Id",
          "default": null,
          "description": "Catalog propeller public id."
        },
        "throttle_pct": {
          "type": "number",
          "title": "Throttle Pct",
          "default": 100,
          "maximum": 100,
          "exclusiveMinimum": 0
        },
        "propeller_label": {
          "anyOf": [
            {
              "$ref": "#/$defs/PropellerLabel"
            },
            {
              "type": "null"
            }
          ],
          "default": null,
          "description": "Use instead of propeller_id to run from the printed size."
        }
      },
      "description": "One powertrain, as the anonymous endpoint accepts it (spec D4).\n\nCatalog components are referenced by their public id (``comp_…``, from\n``search_components``). The propeller may instead be given as a label, which\nis all the Fast model needs."
    }
  },
  "title": "sweep_powertrainArguments",
  "required": [
    "powertrain",
    "sweep"
  ],
  "properties": {
    "sweep": {
      "$ref": "#/$defs/SweepAxis"
    },
    "powertrain": {
      "$ref": "#/$defs/PowertrainInput"
    }
  }
}
    arguments 203 lines
  • estimate_propeller unknown 57m ago

    Thrust, torque and shaft power for one propeller, from its printed size. A closed-form momentum plus blade-element equation — no motor, no battery, no account. Give the size as it is printed: a 10x5 is `diameter_in=10`, `pitch_in=5`. `chord_ratio` is the chord at 75 % radius over the diameter: 0.065 thin electric, 0.07 sport, 0.10 slow flyer, 0.11 multirotor.

    mcp-tool

    {
  "type": "object",
  "title": "estimate_propellerArguments",
  "required": [
    "diameter_in",
    "pitch_in",
    "rpm"
  ],
  "properties": {
    "rpm": {
      "type": "number",
      "title": "Rpm"
    },
    "blades": {
      "type": "integer",
      "title": "Blades",
      "default": 2
    },
    "pitch_in": {
      "type": "number",
      "title": "Pitch In"
    },
    "altitude_m": {
      "type": "number",
      "title": "Altitude M",
      "default": 0
    },
    "camber_pct": {
      "type": "number",
      "title": "Camber Pct",
      "default": 3.2
    },
    "chord_ratio": {
      "type": "number",
      "title": "Chord Ratio",
      "default": 0.065
    },
    "diameter_in": {
      "type": "number",
      "title": "Diameter In"
    },
    "airspeed_m_s": {
      "type": "number",
      "title": "Airspeed M S",
      "default": 0
    }
  }
}
    arguments 48 lines
_ try it through the hub, ceiling 0

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  1. Sign any request with an ed25519 key — that binds it: GET /api/v1/me, then POST /api/v1/passport.
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_ record

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