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Douglas XB-43 Jetmaster

United States (1946)
Picture of Douglas XB-43 Jetmaster Experimental Bomber Aircraft
Picture of Douglas XB-43 Jetmaster Experimental Bomber Aircraft Picture of Douglas XB-43 Jetmaster Experimental Bomber Aircraft
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The three-man Douglas XB-43 Jetmaster existed only through a pair of prototypes - the first flying in May of 1946.


Detailing the development and operational history of the Douglas XB-43 Jetmaster Experimental Bomber Aircraft.  Entry last updated on 5/31/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com

Born from the XB-42 "Mixmaster" program - which sought a unique solution for a budget-conscious medium bomber platform alternative to the large and expensive Boeing B-29 "Superfortress" - the Douglas XB-43 "Jetmaster" was an evolved, jet-powered offshoot of the original design. The earlier XB-42 was powered by a pair of Allison inline engines arranged in a "pusher" setup at the rear of the aircraft which promoted speed gains over a traditional configuration. This left the forward / middle fuselage and wings clear of any mechanical obstructions and resulted in a more streamlined shape. At one point, the XB-42 was fitted with Westinghouse axial-flow turbojets which advanced it along altogether different lines. While neither design was adopted (two prototypes were completed), it did lay the foundation for the XB-43 which substituted the Westinghouse powerplants with a pair of General Electric J35 series engines. Two flyable XB-43 prototypes then emerged.

The XB-43 was more-or-less an add-on project to the in-development XB-42. The airframe proved feasible for the study of jet propulsion in a medium-sized bomber airframe so an agreement between the United States Army Air Force (USAAF) and Douglas Aircraft was had in March of 1944 with World War 2 (1939-1945) still ongoing. The aircraft resembled the XB-42 airframe on the whole while the inline engines were given up for the General Electric turbojets. Engineers added a pair of intakes along either side of the fuselage near the wingroots and exhaust ports took up the space where the propeller units once lay at the rear. The aircraft retained its single dorsal vertical tail fin (the ventral fin was deleted while the dorsal fin was enlarged), retractable tricycle undercarriage, and two-man cockpit arrangement. The nose section was glazed over for a bombardier's position bringing the operating crew total to three. Proposed defensive armament was 2 x 12.7mm heavy machine guns held in a remote-controlled tail turret though this was never fitted. The bomb load was to total 8,000 pounds. An attack variant (possibly designated as "A-43") was entertained that would have fitted multiple machine guns in the nose with the bombardier's position omitted and covered over. Additional weapons support in this version would have been added for underwing rockets.

Due to the limited availability of the GE J35 engines, the XB-43 product languished for several years before the aircraft could be flown. When fitted with its jets the aircraft suffered damage during ground running tests which saw one engine explode. A first flight was finally recorded on May 17th, 1946 but, by this time, World War 2 (1939-1945) had ended and many promising programs fell under the axe of the massive military drawdown that followed. The second prototype (given the developmental designation of "YB-43") followed in flyable form during 1947. The original J35 turbojets were then upgraded with J47 series engines.

The first prototype - s/n 44-61508 - was eventually cannibalized for its useful parts (to serve the second) and given up as a target. The second prototype - s/n 44-61509 managed a rather healthy test life until December of 1953. By this time, the now-USAF (the United States Army Air Force was renamed after World War 2) focused its energies on dedicated jet-powered bomber developments and not simply modified propeller-driven forms. This led to the cancellation of the XB-43 project in whole - the aircraft passed on for preservation to the National Museum of the United States Air Force (Dayton, Ohio).

As completed, the XB-43 exhibited a length of 15.7 meters, a wingspan of 21.7 meters, and a height of 7.4 meters. Its empty weight was 22,900 lb with a Maximum Take-Off Weight (MTOW) of 40,000 lb. Power was originally from 2 x General Electric J35-GE-3 turbojet engines of 4,000 lb thrust each. Maximum speed was recorded to be 507 miles per hour with a range out to 2,500 miles, and a service ceiling nearing 38,500 feet (requiring use of a pressurized crew cabin). Rate-of-climb reached 2,470 feet-per-minute.


Picture of the Douglas XB-43 Jetmaster Experimental Bomber Aircraft
Picture of the Douglas XB-43 Jetmaster Experimental Bomber Aircraft



Any available statistics for the Douglas XB-43 Jetmaster Experimental Bomber Aircraft are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).






Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 750mph
Lo: 375mph
    This entry's maximum listed speed (506mph).

    Graph average of 562.5 miles-per-hour.
City-to-City Ranges
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Graph showcases the Douglas XB-43 Jetmaster's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
2
2


  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


Altitude Visualization
Small airplane graphic
  Compare this entry against other aircraft using our Comparison Tool  
National Flag Graphic
Origin: United States
Year: 1946
Type: Experimental Bomber Aircraft
Manufacturer(s): Douglas Aircraft Company - USA
Production: 2
Global Operators:
United States (cancelled)
Historical Commitments / Honors:

Military lapel ribbon for Operation Allied Force
Military lapel ribbon for the Arab-Israeli War
Military lapel ribbon for the Battle of Britain
Military lapel ribbon for the Battle of Midway
Military lapel ribbon for the Berlin Airlift
Military lapel ribbon for the Chaco War
Military lapel ribbon for the Cold War
Military lapel ribbon for the Cuban Missile Crisis
Military lapel ribbon for the Falklands War
Military lapel ribbon for the French-Indochina War
Military lapel ribbon for the Golden Age of Flight
Military lapel ribbon for the 1991 Gulf War
Military lapel ribbon for the Indo-Pak Wars
Military lapel ribbon for the Iran-Iraq War
Military lapel ribbon for the Korean War
Military lapel ribbon for the 1982 Lebanon War
Military lapel ribbon for the Malayan Emergency
Military lapel ribbon for the attack on Pearl Harbor
Military lapel ribbon for the Six Day War
Military lapel ribbon for the Soviet-Afghan War
Military lapel ribbon for the Spanish Civil War
Military lapel ribbon for the Suez Crisis
Military lapel ribbon for the Vietnam War
Military lapel ribbon for Warsaw Pact of the Cold War-era
Military lapel ribbon for the WASP (WW2)
Military lapel ribbon for the World War 1
Military lapel ribbon for the World War 2
Military lapel ribbon for the Yom Kippur
* Ribbons not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective campaigns/operations.
Measurements and Weights icon
Structural - Crew, Dimensions, and Weights:
Unless otherwise noted the presented statistics below pertain to the Douglas XB-43 Jetmaster model. Common measurements, and their respective conversions, are shown when possible.

Operational
CREW


Personnel
3


Dimension
LENGTH


Feet
51.51 ft


Meters
15.7 m


Dimension
WIDTH


Feet
71.19 ft


Meters
21.7 m


Dimension
HEIGHT


Feet
24.28 ft


Meters
7.4 m


Weight
EMPTY


Pounds
22,884 lb


Kilograms
10,380 kg


Weight
LOADED


Pounds
39,683 lb


Kilograms
18,000 kg

Engine icon
Installed Power - Standard Day Performance:
2 x General Electric J35-GE-3 turbojet engines developing 4,000lb of thrust each.

Performance
SPEED


Miles-per-Hour
506 mph


Kilometers-per-Hour
815 kph


Knots
440 kts


Performance
RANGE


Miles
2,485 mi


Kilometers
4,000 km


Nautical Miles
2,160 nm


Performance
CEILING


Feet
38,386 ft


Meters
11,700 m


Miles
7.27 mi


Performance
CLIMB RATE


Feet-per-Minute
2,470 ft/min


Meters-per-Minute
753 m/min

Supported Weapon Systems:

Graphical image of an aircraft medium machine gun
Graphical image of an aircraft heavy machine gun
Graphical image of an aircraft conventional drop bomb munition
Armament - Hardpoints (0):

PROPOSED (Standard):
2 x 12.7mm heavy machine guns in remote-controlled tail turret.

PROPOSED (Optional):
Up to 8,000lb of conventional drop stores carried.
Variants: Series Model Variants
• XB-43 "Jetmaster" - Base Series Name; 2 prototypes complete.
• YB-43 - U.S. Army designation for XB-43 prototype
• A-43 - Proposed attack form featuring 8 x 12.7mm heavy machine guns in the nose now lacking the bombardier's station.