DC1973
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This is looking beautiful!
Thanks Rick! If I get anywhere near the quality of your work, I'll be more than happy

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The Staff of SOH
This is looking beautiful!
Wow Dean, that's really looking good! On the panel lines I use both maps, and I tend to favor being really subtle. The texture size and how parts are mapped also comes into play.
Much progress over the past two days on the Reporter's textures, thoroughly enjoying it and the almost limitless possibilities available using alphas and specular maps. Probably posting too many images of this development but what the hell...
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I've never noticed to cowlings until now. I thought they were just standard P-61 units, but they're not. It looks like Northrop took some from a B-26 and flipped them over! (I also never noticed the big scoop underneath either. I guess I was just focused on how different the crew pod was!) I wish I could get a hold of Lone Star Model's conversion kit for a Monogram P-61!
That's because the Reporter was based off of the P-61C, not the A or B model.
Based on the information I have, the P-61A and B were very similar and both used the same B-series Pratt & Whitney R-2800 engines producing 2000 horsepower. The P-61B featured a new radar system, necessitating an 8 inch longer nose, various internal systems improvements, a change in the design of the nose wheel door and the addition of a nose wheel mounted taxi light. Aside from the taxi light, nose wheel door, and longer nose, the P-61A and B looked identical.
The P61C development was authorized near the end of 1943 and was to improve the speed and altitude performance. The P-61C was designed to use the newer C-series R-2800-77 turbo supercharged engines that produced 2800 HP. However, the USAAF had ordered so many of these high horsepower C-series engines that production could not meet demands and this delayed the development of the P-61C. The first production P-61C would not come the assembly line until July of 1945. The engine cowling of the P-61C featured carburetor air intakes on both sides, beginning at the very front of the cowl ring, and a large intake at the bottom of the engine nacelle for the turbo supercharger.
The P-61E project was started in the middle of 1944 and was also to develop the P-61 as a long range day fighter/escort aircraft for the Pacific theater. The removal of the 20mm cannons from the belly, the dorsal turret system, and replacement of the radar equipment with four 50 caliber machine guns greatly reduced the weight of the P-61 and improved its speed, but it was still slower than the newly developed P-82 Twin Mustang. Remember the C-series engine shortage? That is why the P-61E used the same 2000 horsepower R-2800-65 B-series engines as the earlier P-61A/B.
The first XF-15 was built from the XP-61E, so it retained the R-2800-65 engines, but the second XF-15 was built from a P-61C. All 36 of the production F-15A's used the 2800 horsepower R-2800-77 like the P-61C.
I hope that clears up some of the engine confusion.
PRIMARY FUNCTION: | Night Fighter |
CONTRACTOR: | Northrop Aircraft Inc. of Hawthorne, California |
UNIT COST: | $170,000 |
CREW: | Pilot, Radar Operator, and Gunner |
FIRST FLIGHT: | May 21, 1942 (XP-61) |
SERVICE DELIVERY: | May 1944 (P-61A) |
FIRST OP MISSION: | July 3, 1944 (Europe) |
FIRST KILL: | July 6, 1944 (Pacific) |
TOTAL PRODUCED: | 706 (all variants) |
ENGINES: | Two Pratt & Whitney R-2800-65 Double Wasp 18-Cylinder engines rated at 2,250 hp |
WING SPAN: | 66 Feet |
LENGTH: | 49 Feet, 7 Inches |
HEIGHT: | 14 Feet, 8 Inches |
MAX. SPEED: | 369 MPH |
HEIGHT: | 14 Feet, 8 Inches |
EMPTY WEIGHT: | 20,965 lb |
MAX. T.O. WEIGHT | 34,200 lb |
SERVICE CEILING: | 33,100 Feet |
MAX. RANGE: | 1,350 Miles, (1,900 miles ferry) |
RATE OF CLIMB: | 2,090 Feet Per Minute |
ARMAMENT: | Four 20 mm Hispano M2 cannons, four Browning M2 .50 caliber heavy machine guns, 6,400 lb of bombs or rockets |
The R-2800-65 was capable of a maximum power output of 2,250 HP, but that was with the water/methanol injection system. The maximum power without the water/methanol injection was 2000 horsepower.
The R-2800-77 was capable of a maximum power output of 2,800 HP with water/methanol injection, but limited to 2400 HP without water injection.
Guess I should have been more precise with the output ratings in my first post. My engine data is from FAA documents.