Difference between revisions of "Minibee TRL2"
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</Gallery> | </Gallery> | ||
| + | |||
| + | == General characteritics == | ||
| + | |||
| + | |||
| + | <ul> | ||
| + | <li><b>Crew</b>: 2 pilots</li> | ||
| + | <li><b>Capacity</b>: from 1 passenger and 1 patient to 3 passengers and 2 patients with central module</li> | ||
| + | <li><b>Length</b>: 6.01 m (19 ft 9 in)</li> | ||
| + | <li><b>Height</b>: 2,3 m (7 ft 7 in)</li> | ||
| + | <li><b>Empty Weight</b>: 850 kg (1,873 lb)</li> | ||
| + | <li><b>Max Take-Off Weight</b>: 1,200 kg (2,643 lb)</li> | ||
| + | <li><b>Powerplant</b>: Piston engine for 250 kW at Take-Off and electric motors</li> | ||
| + | <li><b>Central rotor area</b>: 12,6 m <sup>2</sup> (41.5 sq ft)</li> | ||
| + | <li><b>Wing rotor area</b>: 10,6 m <sup>2</sup> (35 sq ft)</li> | ||
| + | <li><b>Wings Area</b>: 8,66 m<sup>2</sup> (28.5 sq ft)</li> | ||
| + | <li><b>Airfoil</b>: Davis basic B-24 </li> | ||
| + | <li><b>Fuel Capacity</b>: 150 l ()</li> | ||
| + | </ul> | ||
| + | |||
| + | <h3>Performance </h3> | ||
| + | <ul> | ||
| + | <li><b>Cruise speed</b>: 250 km/h (155 mph | 135 kn)</li> | ||
| + | <li><b>Max speed</b>: 300km/h (186 mph | 162 kn)</li> | ||
| + | <li><b>Range</b>: 500 km (311 mi | 270 nm)</li> | ||
| + | <li><b>Service ceiling</b>: 4,000 m (13,000 ft) </li> | ||
| + | <li><b>Rate of climb</b>: 6,45 m/s (1,270 ft/min)</li> | ||
| + | </ul> | ||
| + | |||
| + | </td> | ||
| + | |||
| + | |||
| + | <td> | ||
| + | <div class="floatright"> | ||
| + | |||
| + | |||
| + | </div> | ||
| + | </td> | ||
| + | [[File:Minibeev14_image.png|500px|right]] | ||
| + | </table> | ||
| + | |||
| + | |||
[[Category:MiniBee]] | [[Category:MiniBee]] | ||
[[Category:TRL2]] | [[Category:TRL2]] | ||
Revision as of 11:17, 4 January 2021
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
- INSA : Seat
- 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.
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)
