Encyclopedia Astronautica
Martlet 2G1-1


Solid rocket stage. Mass 130 kg (287 lb).

Status: Development ended 1966.
Gross mass: 130 kg (280 lb).
Unfuelled mass: 21 kg (46 lb).
Height: 3.21 m (10.53 ft).
Diameter: 0.29 m (0.95 ft).
Span: 0.45 m (1.47 ft).

More... - Chronology...


Associated Countries
Associated Launch Vehicles
  • Martlet 2G-1 Canadian gun-launched orbital launch vehicle. The Martlet 2G-1 was the absolute minimum gun-launched satellite vehicle. Conceived when the HARP project was under threat, it was a seven-inch diameter, two-stage solid propellnat vehicle that would be sabot-launched from the HARP 16 inch gun. Its total payload in orbit would have been just two kilogrammes - ideal for today's planned nano-satellites. Unfortunately even this minimum orbital launch vehicle could not be demonstrated before the program was shut down. More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

Home - Browse - Contact
© / Conditions for Use