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TRIMIS

Multibody Advanced Airship for Transport

Project

MAAT - Multibody Advanced Airship for Transport


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Project website:
Duration:
Start date: 01/09/2011,
End date: 01/02/2015

Status: Finished
Funding details:
Total cost:
€5 071 721
EU Contribution:
€3 767 000

Overview

Background & policy context:

Previous research resulted in promising ideas. They offered the prospect of substantial impact and benefit to the air transport system, they were radical rather than evolutionary, they were forward looking rather than immediate in application and they had specific technology challenges.

The MAAT project investigates the concept of a cruiser-feeder system for medium and long range transports. The cruiser being a very large aircraft, which remain airborne for long periods on stable routes around the world, interconnecting major populated centres. The feeders would transfer passengers and freight to/from the cruiser at interception points in flight.

A number of variants (mode of operation, cruiser and feeder air vehicle design) are possible. There is need to study the system and its components in a structured approach. Note that the environmental impact of the feeder/cruiser system could be considerably better than the present system, as fuel consumption could be substantially less.

Objectives:

The MAAT project aims to investigate aerial transportation possibility by airship based cruiser-feeder system. This system is composed of tree modules:

  • the cruiser, named PTAH, (acronym of Photovoltaic Transport Aerial High altitude system);
  • the feeder, named ATEN (Aerial Transport Elevator Network feeder), this is a VTOL system (Vertical Take Off and Landing) which ensures the connection between the cruiser and the ground;
  • the vertical airport hub, named AHA (acronym for Airport Hub for Airship feeders).

The feeder can lift up and down by the control of buoyancy force and displace horizontally to join to cruiser. The project aims to:

  • identify and design the best type of propulsion for the PTAH, a discoid innovative airship able to remain airborne for long periods and to travel great distances, in order to reduce the environmental impact against the present system, as fuel consumption is null, both cruiser and feeder are energetically autonomous by photovoltaic energy and innovative electric propulsion;
  • study the different ways of approaching and joining between ATEN and PTAH, and consequently, the release of ATEN from PTAH;
  • design the best procedure of docking operations thus identified in order to obtain the minimum disruption to passengers and the maximum safety for themselves and for goods.

Furthermore the prokject aims to study the different architectures of PTAH and ATEN, in such a way that:

  • the lift up capacity guaranteed by the buoyancy force, may be accompanied by the power of the engines;
  • effective and safe procedures for docking;
  • ATEN can land and take off from Airport Hubs named AHA located in major populated centres;
  • PTAH satisfies the better possible aerodynamic performances possible for the dimensions and the operative mission.

The project also studies the transfer operations of goods and people between ATEN and PTAH to:

  • minimize distress conditions for passengers;
  • maximize performances especially for goods;
  • enhance safety of these operations to maximum possible level.

To achieve the objectives, the study of the system and components must be highly structured.

Methodology:

Study the cruiser-feeder system and its components in a fully structured ans systemic approach in order to define:

  • the general design of cruiser and feeder, to optimize aerodynamics and photovoltaic energy;
  • the preliminary structural draft of cruiser, feeder and hub;
  • control systems, procedures and codes for stability and flying attitude control;
  • electrical propulsion systems able to overcome the problems related to the low air density;
  • operative procedures for rendezvous and joining operations;
  • internal design of cabins and cargo;
  • study and design of cruiser/feeder connections;
  • passive and active safety systems.

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