Tupolev Tu-144D: Difference between revisions

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m (Link to state overlays.)
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== Current status ==
== Current status ==
Mar 2018.
Sep 2018.


* FDM and control in agreement with POH;
* FDM and control in agreement with POH;
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* [[Mumble|Mumble]] control;
* [[Mumble|Mumble]] control;


* automatic pushback;
* [https://gitlab.com/mdanil/flightgear-autopush Autopush] automatic pushback;


* basic instruments and annunciators in 3d.
* basic instruments and annunciators in 3d.
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== Characteristics and performance ==
== Characteristics and performance ==
{| class="prettytable"
{| class="prettytable"
! colspan="2" align="left" | Mass
! colspan="2" align="left" | Weight
|-
| Empty || 99,200 kg
|-
|-
| Max T/O || 207,000 kg
| Max T/O || 207,000 kg
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| Normal T/O || 180,000 kg
| Normal T/O || 180,000 kg
|-
|-
| Max. landing || 120,000 kg
| Max landing || 120,000 kg
|-
| Fuel max || 98,000 kg
|-
| Payload max || 15,000 kg
|-
|-
! colspan="2" align="left" | Speed
! colspan="2" align="left" | Speed
|-
| Liftoff || 360..380 km/h
|-
|-
| Cruise || Mach 1.9..2.1
| Cruise || Mach 1.9..2.1
|-
|-
| Max speed at 19,000 m || Mach 2.15
| Max at 19,000 m || Mach 2.15
|-
|-
| Pattern || 340 km/h
| Pattern || 340 km/h IAS
|-
|-
| Glideslope || 290 km/h
| Approach || 290 km/h IAS
|-
|-
| Touchdown || 270..290 km/h
! colspan="2" align="left" | Altitude
|-
|-
! colspan="2" align="left" | Altitude
| Cruise || 16,500..19,500 m
|-
|-
| Practical ceiling || 19,700 m
| Practical ceiling || 19,700 m
|-
|-
| Cruise || 16,500..19,500 m
! colspan="2" align="left" | Range
|-
| Max fuel, 7,000 kg payload || 6500 km
|}
|}



Revision as of 14:52, 23 September 2018

Tupolev Tu-144D
Tu 144 preparing for takeoff
Tu 144 preparing for takeoff
Type Airliner, Supersonic aircraft
Configuration Canard aircraft, Delta-wing aircraft
Propulsion Quadjet (Jet aircraft, Four-engine aircraft)
Manufacturer Tupolev
Author(s) @femboywings, @ShFsn, @konsni
FDM JSBSim
--aircraft= Tu-144D
Status Advanced production
 FDM Stars-5.png
 Systems Stars-5.png
 Cockpit Stars-3.png
 Model Stars-5.png
Supports Checklists Tutorials
Development
 Repository The development repository of the Tupolev Tu-144D.
Download Download the Tupolev Tu-144D aircraft package for the current stable release (2020.3).
License CC BY-SA 4.0
This aircraft is NOT available under the GNU GPL 2, the primary license of the FlightGear project. This means that parts cannot be reused in the official FlightGear repositories.
Wikipedia Tupolev Tu-144 This is a link to a Wikipedia article

The Tupolev Tu-144 (NATO: Charger) supersonic transport (SST) was the first of the two supersonic passenger airliners to fly. The other one was the Concorde.

The aircraft is unique for its retractable canards, which enable takeoff/landing at speeds not much higher than those of conventional airliners.

FlightGear model

The project was conceived in July 2014 and has been active since April 2015. Its goal is to accurately model flight dynamics, systems and instruments of the Tu-144 entirely in JSBSim and then make a convincing visual model.

catalog.xml for the QT launcher: https://gitlab.com/mdanil/Tu-144_hangar/raw/master/catalog.xml

Current status

Sep 2018.

  • FDM and control in agreement with POH;
  • reasonable autopilot based on the documentation for Tu-154B;
  • plausible navigation stack with the Orbita-10 FMC, RSBN support, mobile RSBN and mobile Katet landing system;
  • complete set of cockpit warnings;
  • engines, systems and most instruments following POH;
  • automated crew: callouts and landing/RTO actions;
  • correct animation, sounds, view and particle effects in multiplayer;
  • basic damage;
  • basic instruments and annunciators in 3d.

Known issues

  • The visual model needs a replacement;
  • most of the cockpit is still only represented by PUI dialogs.

The reworking of visual will start when the relevant sizes are known from cockpit modeling.

Characteristics and performance

Weight
Empty 99,200 kg
Max T/O 207,000 kg
Normal T/O 180,000 kg
Max landing 120,000 kg
Fuel max 98,000 kg
Payload max 15,000 kg
Speed
Cruise Mach 1.9..2.1
Max at 19,000 m Mach 2.15
Pattern 340 km/h IAS
Approach 290 km/h IAS
Altitude
Cruise 16,500..19,500 m
Practical ceiling 19,700 m
Range
Max fuel, 7,000 kg payload 6500 km

External links