Method for injecting fuel into a combustion chamber of a cylinder of an internal combustion engine of a vehicle, - wherein the fuel is injected with exactly five jets into the combustion chamber by means of injector, - wherein a first plane is defined in which both the central axis of the injector and the central axis of the cylinder lie, and - wherein a second plane is defined in which both the central axis of the injector and the surface normal of the first plane lie, wherein a direction of each of the jets is defined • by a first angle (α) between the central axis of the injector and a projection of the central axis of the respective jet into the second plane, and • by a second angle (β) between the central axis of the injector and a projection of the central axis of the respective jet into the first plane, - wherein the jets comprise a first, a second, a third, a fourth and a fifth jet, wherein - the first angle (α) of the first jet lies in an angle range from -3° to +3° and - the second angle (β) of the first jet lies in an angle range from -3° to +3° and - the first angle (α) of the second jet lies in an angle range from -40° to -20° and - the second angle (β) of the second jet lies in an angle range from -40° to -20° and - the first angle (α) of the third jet lies in an angle range from -20° to -5° and - the second angle (β) of the third jet lies in an angle range from -40° to -20° and - the first angle (α) of the fourth jet lies in an angle range from +5° to +20° and - the second angle (β) of the fourth jet lies in an angle range from -40° to -20° and - the first angle (α) of the fifth jet lies in an angle range from +20° to +40° and - the second angle (β) of the fifth jet lies in an angle range from -40° to -20°, wherein all jets lie outside the profile, projected into the planes, of a valve lift curve and below the profile, projected into the planes, of a curve of the lower edge of a combustion chamber roof. - wherein the fuel is injected with exactly five jets into the combustion chamber by means of injector, - wherein a first plane is defined in which both the central axis of the injector and the central axis of the cylinder lie, and - wherein a second plane is defined in which both the central axis of the injector and the surface normal of the first plane lie, • by a first angle (α) between the central axis of the injector and a projection of the central axis of the respective jet into the second plane, and • by a second angle (β) between the central axis of the injector and a projection of the central axis of the respective jet into the first plane, - wherein the jets comprise a first, a second, a third, a fourth and a fifth jet, wherein - the first angle (α) of the first jet lies in an angle range from -3° to +3° and - the second angle (β) of the first jet lies in an angle range from -3° to +3° and - the first angle (α) of the second jet lies in an angle range from -40° to -20° and - the second angle (β) of the second jet lies in an angle range from -40° to -20° and - the first angle (α) of the third jet lies in an angle range from -20° to -5° and - the second angle (β) of the third jet lies in an angle range from -40° to -20° and - the first angle (α) of the fourth jet lies in an angle range from +5° to +20° and - the second angle (β) of the fourth jet lies in an angle range from -40° to -20° and - the first angle (α) of the fifth jet lies in an angle range from +20° to +40° and - the second angle (β) of the fifth jet lies in an angle range from -40° to -20°,