Encyclopedia Astronautica
Pedro Recruit-1


Solid propellant rocket stage. Thrust 244.00 kN.

Status: Retired 1977.
Height: 3.10 m (10.10 ft).
Diameter: 0.71 m (2.32 ft).
Thrust: 244.00 kN (54,853 lbf).
Burn time: 11 s.
Number: 8 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • Athena RTV American test vehicle. The Athena was designed to simulate the re-entry environment of an intercontinental ballistic missile and was one of the few examples of sustained interstate missile tests within the United States. More...
  • Pedro Recruit American sounding rocket. Air Launch Probe System (ALPS) and Fighter Launched Advanced Materials Experiment (FLAME) were both vehicles that used a Pedro first stage and a Recruit second stage. They were launched from an F-4 fighter aircraft. More...

Associated Manufacturers and Agencies
  • Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. 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...

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