• UNMANNED SYSTEMS EXHIBITION & CONFERENCE
  • 25 - 27 February 2018
  • ADNEC ABU DHABI - UNITED ARAB EMIRATES
ABU DHABI - UAE

Szender Marcin MSP

  • UMEX
  • Air Vehicles and Systems
  • Engineering - General
  • Services - General
  • Unmanned systems
Szender Marcin MSP

MSP launched its activity in 2001, operates in the field of unmanned and manned systems.

MSP is one of the leading entities in the uav system industry in Poland and its brand is recognizable abroad – it is a renowned partner of the company Trac Group/ChromeAlloy from UK for which it

performed equipment for RollsRoys (aircraft turbine engines), it cooperates with Microflown (the Netherlands) in the field of integration and application of uav systems with acoustic sensors.

The company is distinguished by its innovation and versatility of competencies. The participation in international and national R&D projects, which required unconventional solutions, enabled achieving unique experience in design and performance of various aircraft types. MSP has an experience in design and production of flying systems (up to 150 kg) with various drives, among them the first uav plane in Poland which obtained identification numbers. The photogrammetric system based on an uav plane has made ca. 300 photogrammetric missions in Poland for the area ca 350 km2. Almost all system components have been designed and produced by MSP. It has also experience in design and processing of components and equipment of manned aircrafts and a unique experience in research of dynamic characteristics of the designed planes on the basis of flight tests performed on scaled models.

 

MSP holds a license for design and performance and trade of technology of military and police application of dual-purpose goods and the ISO 9001 certificate.

Address

Poligonowa 1/81
Warsaw
04-051
Poland

Website

http://www.uav.com.pl
Contact Exhibitor

Contact Exhibitor


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  • NEO3
    An unmanned photogrammetric airplane ready for LIDAR integration. Features: over 0.5 hour flight endurance, modular aircraft system - different cargo possibilities, large cargo hold volume, powerful and efficient propulsion system, rail launcher (option), autonomous recovery parachute, easy to transport and deploy. Weight: take-off weight: 12 kg (photogrammetric ver.), take-off weight: 15 kg (LIDAR ver.). Modular payload: photogrammetric head (1 or 2 cameras), laser scanning head (LIDAR). Flight performance: range: 10 km, (communication data link dependent), endurance: over 0.5 hour, (payload dependent), (ground resolution: 5 cm, total area covered: 20 km2), speed: 50–120 km/h, 27–65 knots, typical operational altitude: 300–600 m (1000–2000 ft). Launch method: hand-launched (photogrammetric ver.), rail launcher (LIDAR ver.). Recovery method: autonomous or manual landing, recovery parachute (option). Transportation options: 3 bags/cases, bag/case internal dimensions: 1650 x 350 x 275 mm3.
  • NEO2
    An unmanned photogrammetric electric driven airplane. Features: over 1.5 hour flight endurance, modular aircraft system—different cargo possibilities, powerful and efficient propulsion system, easy to transport and deploy. 1 or 2 SONY A7R cameras with 28 mm OR 55 mm CARL ZEISS lens, yaw compensation (standard), roll compensation (option) Weight: take-off weight: 11 kg. Modular payload: photogrammetric head (1 or 2 cameras). Flight performance: range: 10 km, (communication data link dependent), endurance: over 1.5 hour, (payload dependent), (ground resolution: 5 cm, total area covered: 20 km2), speed: 50–120 km/h, 27–65 knots, typical operational altitude: 300–600 m (1000–2000 ft). Launch method: hand-launched. Recovery method: autonomous or manual landing, recovery parachute (option). Transportation options: 3 bags/cases, bag/case internal dimensions: 1350 x 350 x 275 mm3.
  • geoHOVERFLY
    A photogrammetric / volume calculation version of a versatile micro-class VTOL multi-rotor unmanned platform. Fully autonomous flight control: System advantages: easy mission planning, system can be easily modified and upgraded to customers needs, easy to transport and deploy, designed and manufactured in Poland. Specifications: take-off weight: 1.7 kg, operational cruise speed: 5-10 m/s, flight endurance: 25 min, typical operational altitude: 50-150 m (AGL), Payload: vertical camera: 5MP RGB, focal 8.5mm (FOV 65°), global shutter ground resolution: 2 cm/50m; 5 cm/120 m The system comprises an overlay for AgiSoft software for rapid orthomosaic generation and volume calculations (heaps, embankments, excavations, etc.).
  • HAWK MOTH
    A multi-rotor VTOL uav with a large spectrum of applications. Fully autonomous flight control. Payload options: stabilized tracking head, photogrammetry and mapping head, laser scanner (LIDAR), user customized sensor platform. Weight and payload: multirotor empty weight: 8.5 kg, max. payload capability: 4 kg, multirotor max. gross-weight: 16 kg. Flight characteristics: average cruise speed: 5 m/s, maximum cruise speed: 12.5 m/s. An example of a payload: lidar (Yellowscan Surveyor or Riegl miniVUX) and RGB Sony a6000
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