TEDxNayabashi

ProtechnologyJapan

Development Status

We are currently at key elemental technology development phase for unmanned spaceplane.
Key elemental technologies we are focusing on is as follows:
 - Engine : successful detonation in combustion chamber, mechanism to alternate combustion method (between jet and rocket)
 - Vehicle : high-altitude high-velocity flight capability, reentry technology
 - Control : long range remote control, autonomous flight

開発状況

Items

Engine

Pulse Jet Engine

Pulse Detonation Engine

Airframes / Control systems

PDAS-X01

Flight Demonstration Vehicle
Maiden flight on August, 2008

Length: 1475 mm
Wingspan: 1545 mm
Loaded weight: 6.5 kg
Powerplant: Pulse Jet Engine x 2
Fuel type: Gasoline
Max. Altitude: 50 m
Max. Speed: 80 km/h

PDAS-X02

Flying Test Bed (FTB) 
Maiden flight on December, 2010

Length: 3050 mm
Wingspan: 2137 mm
Loaded weight: 30.1 kg
Powerplant: turbojet engine x 1
Fuel type: kerosene
Max. Altitude: 300 m
Max. Speed: 255 km/h

PDAS-X03A

UAV Flight Control Technology Demonstration Vehicle
Maiden flight on March, 2013

Length: 1455 mm
Wingspan: 1778 mm
Loaded weight: 3.5 kg
Powerplant: Electric motor x 1
Fuel type: (Battery)
Max. Altitude: - m
Max. Speed: - km/h

PDAS-X04

UAV Flight Control Technology / Long Range Flight Demonstration Vehicle
Maiden flight on January, 2013

Length: 2286 mm
Wingspan: 3300 mm
Loaded weight: 21.5 kg (MTOW)
Powerplant: 2st 28c Engin x 1
Fuel type: Gasoline
Max. Altitude: - m
Max. Speed: 130 km/h
Cruise Speed: 80 km/h
Endurance: 10 hours (using 4000cc tank)

Shareholders

ANA

HIS

ハウステンボス

みずほキャピタル

オプティマ・ベンチャーズ

Sponsors

AISIN

冷研

株式会社山一ハガネ

タウンワーク

龍馬プロジェクト

MAEDA

ケーエスディー