Matches in DBpedia 2016-04 for { ?s <http://dbpedia.org/property/specfuelcon> ?o }
- Pratt_&_Whitney_JT8D specfuelcon "0.744".
- Pratt_&_Whitney_JT9D specfuelcon "ca 0.6 lb/lbf/hr at M0.8 at".
- Pratt_&_Whitney_PW1120 specfuelcon "*Military thrust: 22.7 mg/ *Full afterburner: 52.65 mg/".
- Pratt_&_Whitney_R-1535_Twin_Wasp_Junior specfuelcon "0.49".
- Pratt_&_Whitney_R-1690_Hornet specfuelcon "0.6".
- Pratt_&_Whitney_R-1830_Twin_Wasp specfuelcon "0.49".
- Progress_D-436 specfuelcon "61".
- Renault_4P specfuelcon "0.186".
- Renault_6P specfuelcon "0.335".
- SNECMA_M45H specfuelcon "0.32".
- Snecma_Olympus_593 specfuelcon "cruise / SL".
- Rolls-Royce_Clyde specfuelcon "0.71".
- Rolls-Royce_Conway specfuelcon "0.87".
- Rolls-Royce_Crecy specfuelcon "0.55".
- Rolls-Royce_Dart specfuelcon "0.581".
- Rolls-Royce_Derwent specfuelcon "1.17".
- Rolls-Royce_Nene specfuelcon "1.06".
- Rolls-Royce_Pegasus specfuelcon "0.76".
- Rolls-Royce_R specfuelcon "0.85".
- Rolls-Royce_RB.44_Tay specfuelcon "1.1".
- Rolls-Royce_RR500 specfuelcon "Take-off : per hour : Maximum continuous : per hour : Normal cruise : per hour".
- Rolls-Royce_Spey specfuelcon "1.95".
- Rolls-Royce_Trent_500 specfuelcon "0.54".
- Rolls-Royce_Trent_700 specfuelcon "0.565".
- Rolls-Royce_Tyne specfuelcon "0.485".
- Rolls-Royce_Welland specfuelcon "1.121".
- Rotax_912 specfuelcon "285".
- SNECMA_14R specfuelcon "0.292".
- SNECMA_Atar_101 specfuelcon "1.05".
- SNECMA_Turbomeca_Larzac specfuelcon "' 73 kg/kN.h , ' 76 kg/kN.h".
- STAL_Dovern specfuelcon "0.009".
- Salmson_AD.3 specfuelcon "250".
- Salmson_air-cooled_aero-engines specfuelcon "328".
- Saroléa_Albatros specfuelcon "0.32".
- Saturn_AL-31 specfuelcon "Dry thrust: 24.6 g/".
- Saturn_AL-31 specfuelcon "Full afterburner: 54.3 g/".
- Shvetsov_ASh-62 specfuelcon "469".
- Shvetsov_ASh-73 specfuelcon "350".
- Shvetsov_ASh-82 specfuelcon "*M-82F: 355 g/hp•h for take-off, 320 g/hp•hr at nominal power *M-82FNV: 360 g/hp•h for take-off, 325 g/hp•hr at nominal power *M-82T: 350 to 325 g/hp•h for take-off, 260 to 280 g/hp•hr at cruise power".
- Snecma_Atar specfuelcon "*103 kg/ military power *207 kg/ with afterburner".
- Snecma_M53 specfuelcon "*0.90 Dry engine thrust *2.10 military thrust".
- Soloviev_D-30 specfuelcon "0.79".
- Sunbeam_Pathan specfuelcon "0.169".
- Train_T specfuelcon "322".
- Tumansky_R-11 specfuelcon "*97 kg/ at idle *242 kg/ with afterburner".
- Tumansky_R-13 specfuelcon "*95 kg/ at idle *213 kg/ with afterburner".
- Tumansky_R-15 specfuelcon "*127 kg/[h·kN] at idle *275 kg/[h·kN] with afterburner".
- Tumansky_R-25 specfuelcon "*93 kg/ at idle *98 kg/ at maximum military power *229 kg/ with afterburner".
- Tumansky_R-29 specfuelcon "**95,8 kg/ at maximum military power **183.5 kg/ with afterburner".
- Tumansky_R-29 specfuelcon "=".
- Tumansky_RD-9 specfuelcon "104".
- Turbomeca_Arbizon specfuelcon "31.44".
- Turbomeca_Bastan specfuelcon "352".
- Turbomeca_Gabizo specfuelcon "1.04".
- Turbomeca_Piméné specfuelcon "1.05".
- ULPower_UL260i specfuelcon "180".
- Volvo_RM12 specfuelcon "**Military thrust: 23.9 mg/Ns **Full afterburner: 50.6 mg/Ns".
- Volvo_RM8 specfuelcon "65".
- Walter_HWK_109-509 specfuelcon "20".
- Walter_M601 specfuelcon "377".
- Walter_Sagitta specfuelcon "0.315".
- West_Engineering_XJ38 specfuelcon "1.7".
- Westinghouse_J30 specfuelcon "1.35".
- Westinghouse_J32 specfuelcon "1.7".
- Westinghouse_J34 specfuelcon "1.04".
- Westinghouse_J40 specfuelcon "0.94".
- Williams_F107 specfuelcon "0.682".
- Williams_F112 specfuelcon "apprx 0.25 lb/".
- Wright_J65 specfuelcon "~".
- Wright_R-1820 specfuelcon "0.6".
- Wright_R-2160_Tornado specfuelcon "0.67".