During his work
on the A-4 (v-2) rocket program, Werner von Braun was interested in applying
rocket propulsion to aircraft. Beginning in 1936, he helped convert some
conventional aircraft (mainly a donated He 112 from Heinkel) to operate
on rocket power. After several spectacular failures, in the Spring of 1937
the He 112V5 was flown to an altitude of 800 m (2625') by test pilot
Erich Warsitz using the He 112's conventional piston engine. The rocket
motor was then ignited, and the He 112V5 (see drawings
and photo below) became the first aircraft to fly solely by a liquid-fueled
(alcohol and liquid-oxygen) rocket. More flights were undertaken, proving
the feasibility of rocket power for aircraft. On July 6, 1939 von Braun
made a proposal to the RLM for a rocket powered VTO (Vertical Take Off)
interceptor.
The von Braun Interceptor was of a fairly conventional outline, with a
cigar-shaped fuselage and straight, tapered wings. All the rocket fuel
(alcohol and liquid-oxygen) was stored in tanks behind the cockpit, and
the rocket engine was located in the rear (see cutaway
view below). A single fin and rudder was fitted, along with straight
tailplanes. The pilot was seated in a pressurized cockpit, with an inner
armored section. Take off was a unique and interesting operation. It was
envisioned that the aircraft would be stored vertically in a hanger/launch
facility along two rails. These could then be wheeled by remote control
to the outside, where they would then be launched (see
diagram below). The target would be located by ground radar, and the
interceptor would then be guided for the first minute by graphite vanes
in the rocket exhaust. The pilot then took manual control and changed the
rocket to cruise using an auxiliary combustion chamber. After the attack,
the von Braun interceptor was to glide back to a landing on the built-in
landing skid. The RLM considered this concept too impractical, due to the
at-the-time exotic fuels which were difficult to produce, store and handle.
Plus, there were the specialized launch facilities that had to be constructed
and maintained.
A second version of this VTO interceptor was designed. It was similar to
the first design, except the tail unit was smaller in area, and the wings
now had rounded ends and also exhibited dihedral. Also, the rocket fuels
had been changed to Visol and SV-Stoff, which were easier to store. The
cockpit area was slightly different (see three views to the left). The
launch procedure had been the biggest change however. The huge launch facility
was dispensed with, now the interceptor was launched from the same truck
that was used to transport it (see diagram below).
Both versions were to be armed with four unnamed guns, located two to a
side in the wing roots.
Although this
project was not adopted, it did influence Eric Bachem, who later designed
and produced his Bachem BP-20 Natter, which was actually flown at least
once.
View Josha Hildwine's von Braun Interceptor images
Span | Length | Height | Loaded Weight | Range | Ceiling | Climbing Speed | Cruising Speed |
8.5 m
27' 10" |
9.3 m
30' 6" |
3.02 m
9' 11" |
5000 kg
11023 lbs |
15 min | 8000 m
26247' |
151 m/sec
496 ft/sec |
700 km/h
435 mph |
Span | Length | Height | Loaded Weight | Range | Ceiling | Climbing Speed | Cruising Speed |
8.6 m
28' 3" |
9.3 m
30' 6" |
3.2 m
10' 6" |
5080 kg
12000 lbs |
15 min | 8000 m
26247' |
143 m/sec
469 ft/sec |
690 km/h
429 mph |
There are no scale models currently of this aircraft |
The von Braun VTO Interceptor
(first design) launch facility
A cutaway view showing the internal
components of the von Braun VTO Interceptor (first design)
Diagram of the launch procedure
for the von Braun VTO Interceptor Data (Second Version)
Heinkel 112V3
April 1939 |
|
von Braun Interceptor
first version |
|
von Braun Interceptor
second version |
Color illustrations and drawings above from
Reichdreams Dossier #9 - VTO Interceptor