Statements (20)
| Predicate | Object | 
|---|---|
| gptkbp:instanceOf | 
                                    
                                        
                                            gptkb:piston_engine
                                        
                                         | 
                            
| gptkbp:countryOfOrigin | 
                                    
                                        
                                            gptkb:Soviet_Union
                                        
                                         | 
                            
| gptkbp:developedBy | 
                                    
                                        
                                            gptkb:Rolls-Royce_Nene
                                        
                                         | 
                            
| gptkbp:diameter | 
                                    
                                        
                                            
                                            1.3 m
                                        
                                        
                                         | 
                            
| gptkbp:feature | 
                                    
                                        
                                            
                                            afterburner
                                        
                                        
                                         | 
                            
| gptkbp:firstFlight | 
                                    
                                        
                                            
                                            1952
                                        
                                        
                                         | 
                            
| gptkbp:fuelType | 
                                    
                                        
                                            
                                            kerosene
                                        
                                        
                                         | 
                            
| gptkbp:length | 
                                    
                                        
                                            
                                            2.6 m
                                        
                                        
                                         | 
                            
| gptkbp:manufacturer | 
                                    
                                        
                                            gptkb:Klimov
                                        
                                         | 
                            
| gptkbp:predecessor | 
                                    
                                        
                                            gptkb:Klimov_VK-1
                                        
                                         | 
                            
| gptkbp:thrust | 
                                    
                                        
                                            
                                            33.1 kN
                                        
                                        
                                         26.5 kN  | 
                            
| gptkbp:type | 
                                    
                                        
                                            
                                            axial-flow turbojet
                                        
                                        
                                         | 
                            
| gptkbp:usedInAircraft | 
                                    
                                        
                                            gptkb:Ilyushin_Il-28
                                        
                                         Mikoyan-Gurevich MiG-15bis (limited) Mikoyan-Gurevich MiG-17F  | 
                            
| gptkbp:weight | 
                                    
                                        
                                            
                                            872 kg
                                        
                                        
                                         | 
                            
| gptkbp:bfsParent | 
                                    
                                        
                                            gptkb:MiG-17F
                                        
                                         | 
                            
| gptkbp:bfsLayer | 
                                    
                                        
                                            
                                            8
                                        
                                        
                                         | 
                            
| https://www.w3.org/2000/01/rdf-schema#label | 
                                    
                                        
                                            
                                            Klimov VK-1F
                                        
                                        
                                         |