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Star 63F

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 63F Part of Star 63 Star-63F Credit: Thiokol Thiokol solid rocket engine. In Production. Provided perigee kick for the McDonnell PAM-D2 system. Another version was the Star 63D (TU-936). AKA: 120-KS-23,520;TE-M-963. Status: In Production. Number: 5 . Thrust: 104.63 kN (23,521 lbf). Gross mass: 4,590 kg (10,110 lb). Unfuelled mass: 326 kg (718 lb). Specific impulse: 297 s. Burn time: 120 s. Height: 1.78 m (5.84 ft). Diameter: 1.60 m (5.20 ft). Perigee motor has successfully completed development and qualification and is in production. It can be offloaded to a propellant weight of 1952 kg. Motor components are of proven design features and material, thus maximizing reliability. Total impulse 1,277,319 kgf-s. Propellant mass fraction 0.929. Country: USA. Propellants: Solid. Agency: Thiokol. Back to top of page 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 © 1997-2019 Mark Wade - Contact © / Conditions for Use

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