SunlitZelkova
Posts: 209
Joined: 3/7/2018 Status: offline
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I am now able to provide the performance data for the attackers as well as other data for the Tu-16. Su-6 -- Soviet Union [-1991] (Frontal Aviation [VVS]), AM-42 engine, 37mm Category: Fixed Wing Type: Attack Length: 9.24 meters Wingspan: 13.5 meters Height: 3.89 meters Crew: 2 Empty weight: 4000kg Max weight: 5534kg Max Payload: 0 kg (assuming payload refers to cargo) OODA cycle: N/A (not familiar with how this is calculated) Aircraft size: Small aircraft (0-12m long) Agility: N/A (in the database, there is a number, I don't know what that number actually refers to or how it is calculated) Average climb rate: 40 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Instantaneous climb rate, S/L: 120 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Take-off/Landing Distance: 410 meters/730 meters TOD/LAD Cockpit visibility: Forward: Average, Sideways: Average, Aft: Average Armor: Fuselage: Rifle Resistant? (I am unsure whether parts of the cockpit qualify as the fuselage. Due to the aircraft's size, half of the plane could be considered to be armored, but it is all around the crew, meaning it could be considered to be the cockpit. Apart from around the cockpit area and the engine, there is no armor (although there is a 6mm steel plate in the propeller spinner/the front of the engine), Cockpit: Rifle Resistant? (The sides have steel plates of 4mm and 6mm thickness, there is a 10mm steel plate between the gunner and the pilot, and there are 12mm and 10mm steel plates protecting the gunner, while there is 64mm bulletproof glass used for the front windows and the rear window for the gunner. Considering the normal engagement distances for 7.62mm/Rifle rounds, and that the armor thickness varies, I don't know what the exact classification within CMANO's armor system would be), Powerplant: Handgun Resistant? (It has 4mm of steel all around, considering the normal engagement distances for 7.62mm/Rifle rounds, I don't know whether that amount of armor would still qualify as "Rifle Resistant" or not) Damage points: N/A (I am unsure how this is calculated) Sensors/EW- 1x Mk1 Eyeball Comms/Datalinks- HF Radio (Secure) UHF Radio (Secure) Signatures- N/A (I am unsure as to how to calculate this) Properties- Bombsight - Basic (Assuming this refers to the pilot's gunsight, for example, being used to aim bombs or rockets, as otherwise, this aircraft has no "conventional" bombsight) Propulsion- 1x Mikulin AM-42 #1 Technical details- Same as IL-10 (assuming performance is based purely on the engine and not the airframe) Performance details for Mikulin AM-42 Same as IL-10 (assuming performance is based purely on the engine and not the airframe) Fuel- Same as IL-10 (I am unable to find the fuel amount for the Su-6) Su-6 -- Soviet Union [-1991] (Frontal Aviation [VVS]), AM-42 engine, 23mm Category: Fixed Wing Type: Attack Length: 9.24 meters Wingspan: 13.5 meters Height: 3.89 meters Crew: 2 Empty weight: 4000kg Max weight: 5534kg Max Payload: 0 kg (assuming payload refers to cargo) OODA cycle: N/A (not familiar with how this is calculated) Aircraft size: Small aircraft (0-12m long) Agility: N/A (in the database, there is a number, I don't know what that number actually refers to or how it is calculated) Average climb rate: 40 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Instantaneous climb rate, S/L: 120 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Take-off/Landing Distance: 410 meters/730 meters TOD/LAD Cockpit visibility: Forward: Average, Sideways: Average, Aft: Average Armor: Fuselage: Rifle Resistant? (I am unsure whether parts of the cockpit qualify as the fuselage. Due to the aircraft's size, half of the plane could be considered to be armored, but it is all around the crew, meaning it could be considered to be the cockpit. Apart from around the cockpit area and the engine, there is no armor (although there is a 6mm steel plate in the propeller spinner/the front of the engine), Cockpit: Rifle Resistant? (The sides have steel plates of 4mm and 6mm thickness, there is a 10mm steel plate between the gunner and the pilot, and there are 12mm and 10mm steel plates protecting the gunner, while there is 64mm bulletproof glass used for the front windows and the rear window for the gunner. Considering the normal engagement distances for 7.62mm/Rifle rounds, and that the armor thickness varies, I don't know what the exact classification within CMANO's armor system would be), Powerplant: Handgun Resistant? (It has 4mm of steel all around, considering the normal engagement distances for 7.62mm/Rifle rounds, I don't know whether that amount of armor would still qualify as "Rifle Resistant" or not) Damage points: N/A (I am unsure how this is calculated) Sensors/EW- 1x Mk1 Eyeball Comms/Datalinks- HF Radio (Secure) UHF Radio (Secure) Signatures- N/A (I am unsure as to how to calculate this) Properties- Bombsight - Basic (Assuming this refers to the pilot's gunsight, for example, being used to aim bombs or rockets, as otherwise, this aircraft has no "conventional" bombsight) Propulsion- 1x Mikulin AM-42 #1 Technical details- Same as IL-10 (assuming performance is based purely on the engine and not the airframe) Performance details for Mikulin AM-42 Same as IL-10 (assuming performance is based purely on the engine and not the airframe) Fuel- Same as IL-10 (I am unable to find the fuel amount for the Su-6) Su-6 -- Soviet Union [-1991] (Naval Aviation [AV-MF]), M-71F engine Category: Fixed Wing Type: Attack Length: 9.24 meters Wingspan: 13.5 meters Height: 3.89 meters Crew: 2 Empty weight: 4100kg Max weight: 5100kg Max Payload: 0 kg (assuming payload refers to cargo) OODA cycle: N/A (not familiar with how this is calculated) Aircraft size: Small aircraft (0-12m long) Agility: N/A (in the database, there is a number, I don't know what that number actually refers to or how it is calculated) Average climb rate: 43 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Instantaneous climb rate, S/L: 129 meters per second (this number is based on the IL-10, the Su-6 with the AM-42 engine apparently had slightly worse performance due to having more armor. I was unable to find a number for the aircraft) Take-off/Landing Distance: 410 meters/730 meters TOD/LAD Cockpit visibility: Forward: Average, Sideways: Average, Aft: Average Armor: Fuselage: Rifle Resistant? (I am unsure whether parts of the cockpit qualify as the fuselage. Due to the aircraft's size, half of the plane could be considered to be armored, but it is all around the crew, meaning it could be considered to be the cockpit. Apart from around the cockpit area, there is no armor), Cockpit: Rifle Resistant? (The sides have steel plates of 4mm and 6mm thickness, there is a 10mm steel plate between the gunner and the pilot, and there are 12mm and 10mm steel plates protecting the gunner, while there is 64mm bulletproof glass used for the front windows and the rear window for the gunner. Considering the normal engagement distances for 7.62mm/Rifle rounds, and that the armor thickness varies, I don't know what the exact classification within CMANO's armor system would be), Powerplant: None? (There is however a 6mm steel plate in the propeller spinner/the front of the engine. It is so small though that I don't know whether it would qualify for making the entire engine considered to be armored) Damage points: N/A (I am unsure how this is calculated) Sensors/EW- 1x Mk1 Eyeball Comms/Datalinks- HF Radio (Secure) UHF Radio (Secure) Signatures- N/A (I am unsure as to how to calculate this) Properties- Bombsight - Basic (Assuming this refers to the pilot's gunsight, for example, being used to aim bombs or rockets, as otherwise, this aircraft has no "conventional" bombsight) Propulsion- 1x Shvetsov M-71F, Piston, Max Speed: 277 knots Technical details- N/A (I am unable to locate this information) Performance details for Mikulin AM-42 N/A (I am unable to locate this information) Fuel- Same as IL-10 (I am unable to find the fuel amount for the Su-6) Performance data for DBID #629 Tu-16 Badger-A (if nothing is listed or a certain category is not there, it is because it is correct and thus does not need to be changed)- All data is from the book titled Tupolev Tu-16: Versatile Cold War Bomber by Yefim Gordon, Dmitriy Kommissarov, and Vladimir Rigmant. Crew: 6 Max Weight: 72000kg Instantaneous Climb Rate, S/L: 22 meters per second with a 57000kg take off weight, 18 meters per second with a 71560kg take off weight Armor: (See below) The crew of the front cabin's seats were protected by varying levels of armor, ranging from 8-25mm thickness, made of plates either made of aluminum or steel. The flight deck's sides were protected by two 6mm steel plates, one on each side. The flight deck floor was protected by two 8mm steel plates and a single 15mm glassfibre-textolite composite plate. The crew of the rear cabin's seats were protected by varying levels of armor ranging from 5-24mm in thickness, made of plates either made of aluminum or steel. The rear cabin was protected in varying levels, made of 5-10mm plates of steel, aluminum, cast magnesium alloy, or a combination of cast magnesium alloy and steel. The glass to the side of the tail gunner each were composed of a single 105mm Triplex glass pane, while the glass to the rear of the gunner (the glass the gunner looks out of if sitting forwards in his seat, aiming to the rear of the plane) was a single 135mm Triplex glass pane. The fuselage and powerplant otherwise were unarmored. Due to these varying levels of thickness, I am unsure as to what the thickness would be considered for the cockpit area. Sensors/EW- The SPO-3 Sirena-3 radar warning receiver should be removed. Early bomber Tu-16s did not have this. Comms/Datalinks- The UHF/VHF Radio (Unsecure) should be removed. It should be replaced by a second individual HF Radio (Unsecure) and an individual VHF Radio (Unsecure). Properties- Probe Refuelling should be removed. Tu-16 bombers did not have this capability until 1957, and even then it was only a few, not all of them. Propulsion- The RD-3Ms should be changed to 2x RD-3. They are Turbojets, the maximum speed possible is 411 knots indicated air speed at 6250 meters. Technical details- Military static thrust at S/L- 8750 kg per engine Military static SFC at S/L- 1.0 kg/h/kg Performance Details for 2x RD-3- Please note I only have speed data for military power. I hope the cruising speed and loiter speed can be adjusted accordingly if I provide the landing speed. The landing speed with a 44000kg landing weight is 120 knots. These numbers assume that all of the speeds in the game and in the database are in indicated airspeed. Altitude Band & Throttle Altitude Speed Fuel consumption Band 1, Military Speed 3657.6 meters 378 knots, 0.56 Mach N/A (data unavailable) Band 2, Military Speed 3657.6-7315.2 meters 382 knots, 0.57 Mach N/A (data unavailable) Note- This is such a broad range of altitude that I just used the data for 5000 meters altitude. The speed at military power at 7000 meters is 394 knots. Band 3, Military Speed 7315.2-10972.8 meters 345 knots, 0.51 Mach N/A (data unavailable) Note- This is such a broad range of altitude that I just used the data for 9000 meters altitude. The speed at military power at 10000 meters is 320 knots. Band 4, Military Speed 10972.8-13716 meters 266 knots, 0.39 Mach N/A (data unavailable) Note- This is such a broad range of altitude that I just used the data for 12000 meters altitude. The Tu-16 had a service ceiling of 12800 meters at nominal power. Data for speed performance at higher altitudes than 12000 meters is not available. Note- The maximum speed at take off power with a 55000kg AUW is 535 knots at 6250 meters. This is in true airspeed however. Fuel- Fuel Type: Aviation Fuel, Quantity: 34360kg Thank you for considering my requests.
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Formerly known as Project2035, TyeeBanzai, and FlyForLenin
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