Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Star 63
Thiokol solid rocket engine. Used in Shuttle, Titan 34D. Used on Delta 7925 launch vehicle. First flight 1990.

AKA: PAM-D2. Status: Active. Number: 104 . Thrust: 107.20 kN (24,100 lbf). Gross mass: 3,697 kg (8,150 lb). Unfuelled mass: 431 kg (950 lb). Specific impulse: 282 s. Burn time: 120 s. Height: 1.83 m (6.00 ft). Diameter: 1.60 m (5.20 ft).

Area Ratio: 27.33.



Subtopics

Star 63D Thiokol solid rocket engine. In Production. Perigee motor with a range of propellant loads, yielding GTO payloads from 3,080 to 4,588 pounds at a constant velocity of 8,012 feet per second.

Star 63F Thiokol solid rocket engine. In Production. Provided perigee kick for the McDonnell PAM-D2 system. Another version was the Star 63D (TU-936).

Country: USA. Launch Vehicles: Delta 7925, Delta 7925-10L. Propellants: Solid. Stages: Star 63. Agency: Thiokol.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use