Minibee TRL2

Work done during TRL2

Current universities and schools working on the project

• Centrale Supelec : aeronautical simulation
  

File:201706 pres ECP aero.pdf
File:Suivi code 2017 3.0.pdf
File:Guide fonction code Version 1.0 ECP2016.pdf

• Estaca : Usages and engines
  

File:Rapport projet 5A Mini Bee intérieur.pdf
File:Masse Coûts approx Mini-Bee version ambulance.xlsx
File:2017 01 24 Planches VIP.pdf
File:Rapport projet Mini-Bee.pdf

File:BEE-PLANE REPORT 2016-2017 ISIEB v2.pdf

• Estaca SQY 4A : structure
  

File:RapportdeProjet structure estaca 4A 2017.pdf
File:RapportdeProjet1ersemestre.pdf
File:Soutenance 132F01.pdf
File:Soutenance du 2ème semestre (21F042F2017).pdf

• Supmeca : Structural and mechanical mock-up
  

File:SUPMECA FINAL 201706Bourget.pdf
File:Supmeca MotorisationMiniBee 201706Bourget.pdf
File:Mini-Bee Project 2017 - Aerodynamic optimisation.pdf
File:Présentation Mini-Bee optimisation aérodynamique 2017.pdf
File:Mini-bee soutenance2302 final.pdf
File:Rapport Mini-Bee v5-finale.pdf

• Ensta Bretagne
  

File:ENSTA Bretagne 201706Bourget.pdf

• Polito : equipements
  

File:Final Report Polito 23 02 17.pdf
File:Polito Supmeca presentation 23 02 17.pdf

• Ensta Bretagne : Scale flying mock-up
  

• ENSEA : Human interface
  

File:ENSEA 201706Bourget.pdf

• INSA : Seat
  

File:INSA pres NAE.pdf

• IUT Le Havre : Tilt
  

File:IUT LeHavre 201706Bourget.pdf

• IUT Rouen : capteur et intégration CEM
  

File:CEM IUT Rouen 201706Bourget.pdf
File:IUT Rouen Capteur 201706Bourget.pdf
File:Présentation24-06-17-2 IUT ROUEN 201706Bourget.pdf

• IUT Caen : Rotors and optimisation of power chain
  

File:IUT CAEN PstBgt 201706Bourget.pdf

• Esitech
  

File:ESITECH 201706Bourget.pdf

• Lycée Diderot : rear landing gear

File:Projet Personnelle Mini Bee Sagithan DEVAKUMARAN.pdf
File:Rapport de projet partie personelle SZASZ.pdf File:DIDEROT 201706Bourget.pdf

Mock-Up display

3D mock-up :
3D Mock-up by Hamza Fouatih

Mini-Bee configuration for TRL2.

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General characteritics

• Crew: 2 pilots
• Capacity: from 1 passenger and 1 patient to 3 passengers and 2 patients with central module
• Length: 6.01 m (19 ft 9 in)
• Height: 2,3 m (7 ft 7 in)
• Empty Weight: 850 kg (1,873 lb)
• Max Take-Off Weight: 1,200 kg (2,643 lb)
• Powerplant: Piston engine for 250 kW at Take-Off and electric motors
• Central rotor area: 12,6 m ² (41.5 sq ft)
• Wing rotor area: 10,6 m ² (35 sq ft)
• Wings Area: 8,66 m² (28.5 sq ft)
• Airfoil: Davis basic B-24
• Fuel Capacity: 150 l ()

Performance

• Cruise speed: 250 km/h (155 mph | 135 kn)
• Max speed: 300km/h (186 mph | 162 kn)
• Range: 500 km (311 mi | 270 nm)
• Service ceiling: 4,000 m (13,000 ft)
• Rate of climb: 6,45 m/s (1,270 ft/min)