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Signed-off-by: Douglas Schilling Landgraf <[email protected]>
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...hare/vss-lib/airspace-vehicles/rockets/NASA/Space_Launch_System/space_launch_system.vspec
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| # Licensed under the Apache License, Version 2.0 (the "License"); | ||
| # you may not use this file except in compliance with the License. | ||
| # You may obtain a copy of the License at | ||
| # | ||
| # http://www.apache.org/licenses/LICENSE-2.0 | ||
| # | ||
| # Unless required by applicable law or agreed to in writing, software | ||
| # distributed under the License is distributed on an "AS IS" BASIS, | ||
| # WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied. | ||
| # See the License for the specific language governing permissions and | ||
| # limitations under the License. | ||
| # | ||
| Vehicle: | ||
| Type: Rocket | ||
| Vendor: NASA | ||
| Model: Space Launch System (SLS) | ||
| Year: 2024 | ||
| Signals: | ||
| Propulsion: | ||
| EngineThrust: | ||
| datatype: float | ||
| unit: kilonewtons | ||
| description: Thrust produced by the RS-25 engines | ||
| FuelFlowRate: | ||
| datatype: float | ||
| unit: kilograms_per_second | ||
| description: Fuel flow rate to the RS-25 engines | ||
| OxidizerFlowRate: | ||
| datatype: float | ||
| unit: kilograms_per_second | ||
| description: Oxidizer flow rate to the RS-25 engines | ||
| ChamberPressure: | ||
| datatype: float | ||
| unit: bar | ||
| description: Pressure in the RS-25 engine combustion chambers | ||
| EngineTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature of the RS-25 engines during operation | ||
| BoosterThrust: | ||
| datatype: float | ||
| unit: kilonewtons | ||
| description: Thrust produced by the solid rocket boosters | ||
| Flight: | ||
| Altitude: | ||
| datatype: float | ||
| unit: kilometers | ||
| description: Current altitude of the rocket | ||
| Velocity: | ||
| datatype: float | ||
| unit: meters_per_second | ||
| description: Current velocity of the rocket | ||
| Acceleration: | ||
| datatype: float | ||
| unit: meters_per_second_squared | ||
| description: Current acceleration of the rocket | ||
| Heading: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Heading direction of the rocket | ||
| Pitch: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Pitch angle of the rocket | ||
| Roll: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Roll angle of the rocket | ||
| Yaw: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Yaw angle of the rocket | ||
| Fuel: | ||
| FuelLevel: | ||
| datatype: float | ||
| unit: percent | ||
| description: Remaining fuel level in the core stage tanks | ||
| OxidizerLevel: | ||
| datatype: float | ||
| unit: percent | ||
| description: Remaining oxidizer level in the core stage tanks | ||
| Stage: | ||
| CoreStageSeparationStatus: | ||
| datatype: bool | ||
| description: True if the core stage has separated | ||
| BoosterSeparationStatus: | ||
| datatype: bool | ||
| description: True if the solid rocket boosters have separated | ||
| Safety: | ||
| TemperatureWarning: | ||
| datatype: bool | ||
| description: True if any system temperature exceeds safe limits | ||
| PressureWarning: | ||
| datatype: bool | ||
| description: True if any critical pressure exceeds safe limits | ||
| EmergencyAbortStatus: | ||
| datatype: bool | ||
| description: True if an emergency abort sequence has been initiated | ||
| Communication: | ||
| TelemetrySignalStrength: | ||
| datatype: float | ||
| unit: percent | ||
| description: Strength of the telemetry signal to ground control | ||
| CommandStatus: | ||
| datatype: string | ||
| description: Status of the command uplink (Nominal, Delayed, Failed) | ||
| Navigation: | ||
| GPSLatitude: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Latitude from GPS tracking | ||
| GPSLongitude: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Longitude from GPS tracking | ||
| GPSAltitude: | ||
| datatype: float | ||
| unit: kilometers | ||
| description: Altitude from GPS tracking | ||
| Battery: | ||
| BatteryVoltage: | ||
| datatype: float | ||
| unit: volts | ||
| description: Voltage of onboard battery systems | ||
| BatteryTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature of onboard batteries | ||
| Payload: | ||
| PayloadTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature inside the payload bay | ||
| PayloadDoorStatus: | ||
| datatype: bool | ||
| description: True if payload doors are open | ||
| Recovery: | ||
| ParachuteDeploymentStatus: | ||
| datatype: bool | ||
| description: True if parachutes have deployed for the core stage |
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usr/share/vss-lib/airspace-vehicles/rockets/SpaceX/Falcon_9/falcon_9.vspec
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| # Licensed under the Apache License, Version 2.0 (the "License"); | ||
| # you may not use this file except in compliance with the License. | ||
| # You may obtain a copy of the License at | ||
| # | ||
| # http://www.apache.org/licenses/LICENSE-2.0 | ||
| # | ||
| # Unless required by applicable law or agreed to in writing, software | ||
| # distributed under the License is distributed on an "AS IS" BASIS, | ||
| # WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied. | ||
| # See the License for the specific language governing permissions and | ||
| # limitations under the License. | ||
| # | ||
| Vehicle: | ||
| Type: Rocket | ||
| Vendor: SpaceX | ||
| Model: Falcon 9 | ||
| Year: 2024 | ||
| Signals: | ||
| Propulsion: | ||
| EngineThrust: | ||
| datatype: float | ||
| unit: kilonewtons | ||
| description: Current thrust produced by each Merlin engine | ||
| FuelFlowRate: | ||
| datatype: float | ||
| unit: kilograms_per_second | ||
| description: Rate of fuel consumption in kilograms per second | ||
| OxidizerFlowRate: | ||
| datatype: float | ||
| unit: kilograms_per_second | ||
| description: Rate of oxidizer consumption in kilograms per second | ||
| ChamberPressure: | ||
| datatype: float | ||
| unit: bar | ||
| description: Pressure inside the combustion chamber of each engine | ||
| EngineTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature of each engine during operation | ||
| EngineStatus: | ||
| datatype: string | ||
| description: Status of each Merlin engine (Nominal, Shutdown, Failure) | ||
| Flight: | ||
| Altitude: | ||
| datatype: float | ||
| unit: kilometers | ||
| description: Current altitude of the rocket | ||
| Velocity: | ||
| datatype: float | ||
| unit: meters_per_second | ||
| description: Current velocity of the rocket | ||
| Acceleration: | ||
| datatype: float | ||
| unit: meters_per_second_squared | ||
| description: Current acceleration of the rocket | ||
| Heading: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Current heading of the rocket in degrees | ||
| Pitch: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Pitch angle of the rocket | ||
| Roll: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Roll angle of the rocket | ||
| Yaw: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Yaw angle of the rocket | ||
| Fuel: | ||
| FuelLevel: | ||
| datatype: float | ||
| unit: percent | ||
| description: Remaining fuel level as a percentage of total capacity | ||
| OxidizerLevel: | ||
| datatype: float | ||
| unit: percent | ||
| description: Remaining oxidizer level as a percentage of total capacity | ||
| Stage: | ||
| StageSeparationStatus: | ||
| datatype: bool | ||
| description: True if stage separation has occurred | ||
| Stage1LandingStatus: | ||
| datatype: bool | ||
| description: True if the first stage has landed successfully | ||
| Safety: | ||
| TemperatureWarning: | ||
| datatype: bool | ||
| description: True if the rocket's systems are exceeding safe temperature limits | ||
| PressureWarning: | ||
| datatype: bool | ||
| description: True if any critical pressure readings exceed safe levels | ||
| EmergencyAbortStatus: | ||
| datatype: bool | ||
| description: True if an emergency abort sequence has been initiated | ||
| Communication: | ||
| TelemetrySignalStrength: | ||
| datatype: float | ||
| unit: percent | ||
| description: Signal strength of the telemetry data transmission | ||
| CommandStatus: | ||
| datatype: string | ||
| description: Status of ground-to-rocket command transmission (Nominal, Delayed, Failed) | ||
| Navigation: | ||
| GPSLatitude: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Latitude of the rocket's position via GPS | ||
| GPSLongitude: | ||
| datatype: float | ||
| unit: degrees | ||
| description: Longitude of the rocket's position via GPS | ||
| GPSAltitude: | ||
| datatype: float | ||
| unit: kilometers | ||
| description: Altitude above the Earth's surface from GPS data | ||
| Recovery: | ||
| ParachuteDeploymentStatus: | ||
| datatype: bool | ||
| description: True if parachutes have deployed for recovery | ||
| DroneShipLandingStatus: | ||
| datatype: bool | ||
| description: True if the rocket has successfully landed on the drone ship | ||
| Battery: | ||
| BatteryVoltage: | ||
| datatype: float | ||
| unit: volts | ||
| description: Current voltage of the rocket's onboard battery systems | ||
| BatteryTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature of the onboard battery system | ||
| Payload: | ||
| PayloadTemperature: | ||
| datatype: float | ||
| unit: celsius | ||
| description: Temperature of the payload compartment | ||
| PayloadDoorStatus: | ||
| datatype: bool | ||
| description: True if the payload doors are open |