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 30C
Part of Star 30 Family
Star-30C
Star-30C
Credit: Thiokol
Thiokol solid rocket engine. AS 3000. In Production. Apogee motor used for the RCA G-STAR and Martin Marietta series 3000 telecom satellites.

AKA: 51-KS-7,340;TE-M-700-18. Status: In Production. Number: 10 . Thrust: 32.60 kN (7,329 lbf). Gross mass: 630 kg (1,380 lb). Unfuelled mass: 39 kg (85 lb). Specific impulse: 287 s. Burn time: 51 s. Height: 1.49 m (4.90 ft). Diameter: 0.76 m (2.50 ft).

The design incorporates a case cylinder 5 inches longer than the STAR 30BP and an 89-percent-solids HTPB propellant in a 6AI-4V titanium case insulated with silica-filled EPDM rubber. It has a contoured nozzle with an integral toroidal igniter and a carbon-phenolic exit cone. Total impulse 171,002 kgf-s. Propellant mass fraction 0.939.

Propellant Formulation: HTPB.



Country: USA. Spacecraft: AS 3000. Propellants: Solid. 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