Encyclopedia Astronautica
INTA-300-1


Solid rocket stage. 137.00 kN (30,799 lbf) thrust. Mass 300 kg (661 lb).

Status: Retired 1994.
Gross mass: 300 kg (660 lb).
Unfuelled mass: 72 kg (158 lb).
Height: 3.60 m (11.80 ft).
Diameter: 0.26 m (0.85 ft).
Thrust: 137.00 kN (30,798 lbf).
Burn time: 3.10 s.
Number: 6 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • INTA-300 Spanish sounding rocket. Two stage vehicle consisting of 1 x Heron + 1 x Snipe More...
  • Fulmar British sounding rocket. Two stage vehicle consisting of 1 x Heron (107 kN) + 1 x Snipe (16.7 kN). More...
  • INTA-300B Spanish sounding rocket. Later version for heavier payloads fired in 1993-1994. More...

Associated Manufacturers and Agencies
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