See commented-out lines:
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// vehicle data structure is inconsistant and that breaks this https://github.com/r-spacex/SpaceX-API/issues/53 |
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//"size": `The ${data.name} is ${data.height.meters} meters tall and ${data.diameter.meters} meters in diameter. It has a dry mass of ${data.mass.kg} kilograms. `, |
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"leo_weight": `The ${data.name} can launch ${data.payload_weights[0].kg} kilograms to ${data.payload_weights[0].name}`, |
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//engine data structure in the API differs over different vehicles. https://github.com/r-spacex/SpaceX-API/issues/53 |
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//"gto_weight": `The ${data.name} can launch ${data.payload_weights[1].kg} kilograms to ${data.payload_weights[1].name}`, |
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//"mars_weight": `The ${data.name} can launch ${data.payload_weights[2].kg} kilograms to ${data.payload_weights[2].name}`, |
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"first_stage_reusable": `The ${data.name} is ${data.first_stage.reusable? "":"not "}a reusable rocket`, |
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//"engines":`The first stage has ${data.first_stage.engines.number} ${data.engines.type} ${data.engines.version}s. The second stage has ${data.second_stage.engines.number} ${data.second_stage.engines.type}s. `, |
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//"engine_stats":`The first stage's ${data.engines.number} ${data.first_stage.engines.type}s can burn for ${data.first_stage.burn_time_sec} with a sea level thrust of ${data.first_stage.engines.thrust_sea_level} and a vacuum thrust of ${data.first_stage.engines.thrust_vacuum}. The second stage's ${data.second_stage.engines.number} ${data.second_stage.engines.type}s can burn for ${data.second_stage.burn_time_sec} with a sea level thrust of ${data.second_stage.engines.thrust_sea_level} and a vacuum thrust of ${data.second_stage.engines.thrust_vacuum}. `, |
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//"fuel":`The first satge on the ${data.name} carries ${data.first_stage.fuel_amount_tons} tons of ${data.first_stage.engines.propellant_1} and ${data.first_stage.engines.propellant_2}, The second satge on the carries ${data.second_stage.fuel_amount_tons} tons of ${data.second_stage.engines.propellant_1} and ${data.second_stage.engines.propellant_2}. `, |
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"second_stage_payload_options":`${data.second_stage.payloads.option_1} and ${data.second_stage.payloads.option_2}`, |
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"fairing_size":` The fairing is ${data.second_stage.payloads.composite_fairing.height.meters} meters tall and ${data.second_stage.payloads.composite_fairing.diameter.meters} meters in diameter. `, |
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//"engine_loss_max":`${data.engines.engine_loss_max} can be lost during flight without causing mission failure`, |
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//"landing_legs":`The ${data.name} has ${data.landing_legs.number} landing legs which are made from ${data.landing_legs.material}`, |
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// |
Related to issue r-spacex/SpaceX-API#53.
Could use various if statements to handle it, but would only be a temporary fix as it is in the pipeline to be done on the API end. Best to wait until data-structure is near-final.
