Tupolev Tu-144D

From FlightGear wiki
Revision as of 12:32, 14 November 2016 by Anonymous1 (talk | contribs) (Status update.)
Jump to navigation Jump to search
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 is active since April 2015. Its goal is to implement accurate flight dynamics and systems of the Tu-144 entirely in JSBSim (and ultimately support testing in standalone JSBSim), as well as a clean and simple visual model.

Current status

As of November 2016, we have:

  • Plausible FDM and control;
  • Reasonable autopilot, based on the documentation for a related system, ABSU-154;
  • Engines and basic systems following POH;
  • Agreement with known flight envelope and centre of gravity in most configurations;
  • Correct multiplayer visual and sounds.

Known issues

When FDM and systems reach sufficient realism, the following problems will be addressed first.

  • External visual model is still unfinished;
  • There are very few instruments in the cockpit, user having to rely on dialogs.

Characteristics and performance

Mass
Max T/O 207,000 kg
Normal T/O 180,000 kg
Landing 120,000 kg
Speed
Liftoff 390 km/h
Cruise Mach 2.1
Max speed at 19,000 m Mach 2.15
Pattern 340 km/h
Glideslope 290 km/h
Touchdown 270–290 km/h
Altitude
Practical ceiling 19,700 m
Cruise 19,500 m

External links