Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing
<|begin_of_text|><|start_header_id|>system<|end_header_id|> You are a research archivist expert in dataset metadata. Answer the question truthfully.  <|eot_id|><|start_header_id|>user<|end_header_id|> Here is the Description of a dataset. Description:'The purpose of this project is to examine and describe the regulations of microlight aircraft. The national rules of mostly European countries are described in more detail and are compared to the German rules. Most important among the regulations is the maximum take-off mass. In some countries, the limit of 472.5 kg has been raised recently to 600 kg. The report leads from microlight regulations to preliminary sizing of microlight aircraft. Preliminary sizing is based on statistical parameters, which are evaluated for typical microlight aircraft. The parameter k_APP relates landing field length to approach speed. From microlight statistics it was determined an average value k_APP = 2.149 m^0.5/s. The parameter k_TO helps to determine the ratio of power-to-mass and wing loading. An average value k_TO = 1.915 m³/kg was determined. The glid' . Please return only a json list of at most 3 Keywords corresponding to the Description:.<|eot_id|><|start_header_id|>assistant<|end_header_id|> {"Answer" : ["Airplanes","Airplanes--Performance","Design","Ultraleichtflugzeug","Ultralight aircraft"]} <|eot_id|>
 Here is the Description of a dataset. Description:'The purpose of this project is to examine and describe the regulations of microlight aircraft. The national rules of mostly European countries are described in more detail and are compared to the German rules. Most important among the regulations is the maximum take-off mass. In some countries, the limit of 472.5 kg has been raised recently to 600 kg. The report leads from microlight regulations to preliminary sizing of microlight aircraft. Preliminary sizing is based on statistical parameters, which are evaluated for typical microlight aircraft. The parameter k_APP relates landing field length to approach speed. From microlight statistics it was determined an average value k_APP = 2.149 m^0.5/s. The parameter k_TO helps to determine the ratio of power-to-mass and wing loading. An average value k_TO = 1.915 m³/kg was determined. The glid' . Please return only a json list of at most 3 Keywords corresponding to the Description:.
The purpose of this project is to examine and describe the regulations of microlight aircraft. The national rules of mostly European countries are described in more detail and are compared to the German rules. Most important among the regulations is the maximum take-off mass. In some countries, the limit of 472.5 kg has been raised recently to 600 kg. The report leads from microlight regulations to preliminary sizing of microlight aircraft. Preliminary sizing is based on statistical parameters, which are evaluated for typical microlight aircraft. The parameter k_APP relates landing field length to approach speed. From microlight statistics it was determined an average value k_APP = 2.149 m^0.5/s. The parameter k_TO helps to determine the ratio of power-to-mass and wing loading. An average value k_TO = 1.915 m³/kg was determined. The glid
Airplanes; Airplanes--Performance; Design; Ultraleichtflugzeug; Ultralight aircraft