&sq=Qlik&lang=&file=File:Northern_Light_Lander_Mars1.jpg) Northern Light Lander on Mars (artist's impression) | |
| Mission type | Mars rover |
|---|---|
| Operator | Northern Light Consortium |
| Website | www |
| Spacecraft properties | |
| Manufacturer | Thoth Technology |
| Landing mass | 35 kilograms (77 lb) 6 kilograms (13 lb) lander |
| Start of mission | |
| Launch date | cancelled |
Northern Light was a concept mission for a robotic mission to Mars that would consist of a lander and a rover, being studied by a consortium of Canadian universities, companies and organisations. The primary contractor for the spacecraft was Thoth Technology Inc.
The spacecraft would consist of four parts: an apogee kick engine to provide orbital injection for a cruise vehicle that carries the Northern Light lander and the Beaver Rover to a direct rendezvous with Mars using a Hohmann transfer orbit. Atmospheric entry would be achieved by a heat shield, parachute and airbag deployment system. The lander would transfer the rover to the Martian surface. Once deployed on the Martian surface, the lander contacts Earth directly to the 46 m parabolic antenna located at the Algonquin Radio Observatory.
The Beaver Rover was proposed to have a maximum range of 1000 metres (0.62 mile) from the landing site. It would have operated under battery, utilizing tools and sensors to investigate surface rocks that may contain the presence of photosynthetic life.