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Aviation / Aerospace


BMW Strahljager II (P.II)


Single-Seat, Single-Engine Jet Fighter Proposal [ 1946 ]



The Strahljager P.II was the second of four jet-powered fighter designs drawn up by engine-maker BMW during the latter-half of World War 2.



Authored By: Staff Writer | Last Edited: 08/26/2022 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

VIEW SPECIFICATIONS [+]
The second of four "Strahljager" single-seat, single-engine fighter designs promoted by engine-maker BMW was recognized simply as "Projekt II". This offering reversed a few of the design decisions of the earlier P.I detailed elsewhere on this site but relocating the dorsal engine placement to the ventral line, employing a more conventional single-finned tail unit, and positioning the pilot in the prone position. The unique prone approach offered a considerably smaller footprint for the fighter, which would have carried the company's own BMW 003 turbojet engine for power, and theoretically would have allowed the pilot's body to incur forces at higher angles of attack.

The mainplanes were set just ahead of midships and the horizontal planes mounted at the midway point of the tailfin. Sweepback was only apparent along the wing's leading edge. With the engine's placement at the belly of the design, a straight-through configuration meant reduced ductwork and force-defeating turns. The intake sat at the nose with the exhaust port seen just under the tail stem (forcing the empennage to be slightly raised as a result). To round things out, a retractable tricycle undercarriage was to be featured for ground-running.

Like the P.I before it, the P.II would have featured 2 x 30mm MK 108 automatic cannons as primary armament, these seated in the wings (one gun to a wing) due to the small profile nose section dominated by the air intake as well as the cockpit itself.

Like the P.I, the P.II was not furthered beyond its paper stage.©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.

Specifications



Bayerische Motoren Werke / Bavarian Motor Works (BMW) - Nazi Germany
Manufacturer(s)
Nazi Germany
Operators National flag of modern Germany National flag of Nazi Germany
1946
Service Year
Nazi Germany
National Origin
Cancelled
Project Status
1
Crew
0
Units


AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
INTERCEPTION
Ability to intercept inbound aerial threats by way of high-performance, typically speed and rate-of-climb.
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.


29.5 ft
(9.00 meters)
Length
24.4 ft
(7.43 meters)
Width/Span
8.4 ft
(2.57 meters)
Height
3,417 lb
(1,550 kilograms)
Empty Weight
6,063 lb
(2,750 kilograms)
Maximum Take-Off Weight
+2,646 lb
(+1,200 kg)
Weight Difference
monoplane / shoulder-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Shoulder-Mounted
Mainplanes are mounted at the upper section of the fuselage, generally at the imaginary line intersecting the pilot's shoulders.
Straight
The planform involves use of basic, straight mainplane members.


1 x BMW 003 turbojet engine developing between 1,345lb and 1,750lb of thrust.
Propulsion
562 mph
(905 kph | 489 knots)
Max Speed
488 mph
(785 kph | 424 knots)
Cruise Speed
+75 mph
(+120 kph | 65 knots)
Speed Difference
41,010 ft
(12,500 m | 8 miles)
Ceiling
590 miles
(950 km | 513 nm)
Range
4,325 ft/min
(1,318 m/min)
Rate-of-Climb


MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


PROPOSED / ASSUMED:
2 x 30mm MK 108 internal automatic cannons.


0
Hardpoints


Strahljager P.1 - Base Project Designation.
Strahljager P.2 - Second form with underslung engine placement, prone cockpit position; conventional tail unit; high-mounted mainplanes..
Strahljager P.3 - Third iteration; twin-boom (unconnected) layout with inward-canted tailplanes.
Strahljager P.4 - Dimensionally larger and heavier offering; ventral engine placement; conventional tail unit; swept-back mainplanes seated ahead of midships.


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