The second P.1068.01 design was basically the same as the first design (He P.1068.01-78), except six jet engines were to be mounted on the wing leading edge. These could be either the He S 011 or Jumo 004C turbojets. A remote-controlled rear gun turret was to be fitted in the P.1068.01-80's final design variation. This design had the worst aerodynamic layout of all the P.1068.01 designs, found in subsequent windtunnel testing.

Span |
Length |
Height |
Wing Area |
Fuselage Width |
Wheel Track |

19 m
62' 4" |
20 m
65' 7" |
2.1 m
6' 11" |
60 m²
645.84 ft² |
1.8 m
5' 11" |
3.3 m
10' 10" |

Empty Weight |
Fuel |
Lubricants |
Crew |
Load |
Max. Load |
Takeoff Weight |
Wing Loading |

14800 kg
32628 lbs |
7000 kg
15432 lbs |
170 kg
375 lbs |
200 kg
441 lbs |
1500 kg
3307 lbs |
8700 kg
19180 lbs |
23500 kg
51808 lbs |
391.66 kg/m²
80.21 lbs/ft² |

Max. Speed |
Rate of Climb |
Service Ceiling |
Range |
Takeoff Run |
Landing Speed |

930 km/h @ sea level
578 mph @ sea level ------------------------- 896 km/h @ 6000 m 556 mph @ 19685' ------------------------- 850 km/h @ 10000 m 528 mph @ 32808' ------------------------- 835 km/h @ 12000 m 518 mph @ 39370' |
33 m/sec
108 ft/sec |
13200 m
43307 ft |
550 km @ sea level
342 miles @ sea level ------------------------- 830 km @ 6000 m 516 miles @ 19685' ------------------------- 1170 km @ 10000 m 727 miles @ 32808' ------------------------- 1430 km @ 12000 m 858 miles @ 39370' |
900 m
2953' |
166 km/h
103 mph |