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
Talos Mk 11 Mod 2
Hercules solid rocket engine. Talos motor fitted with a conical adapter for mating to the second stage. Solid propellant rocket stage. The Talos motor was fitted with a conical adapter for mating to the second stage. Differential drag forces caused separation. Four fins were arranged at the aft end in a cruciform configuration and drove the vehicle to approximately one revolution per second burnout roll rate. Talos first stage.

AKA: Talos-1. Status: Active. Thrust: 516.00 kN (116,001 lbf). Gross mass: 1,500 kg (3,300 lb). Burn time: 5.20 s. Height: 3.40 m (11.10 ft). Diameter: 0.76 m (2.49 ft).

The Talos motor was fitted with a conical adapter for mating to the second stage. Differential drag forces caused separation. Four fins were arranged at the aft end in a cruciform configuration and drove the vehicle to approximately one revolution per second burnout roll rate.



Country: USA. Launch Vehicles: Talos, Tater, Super Chief II, Talos Sergeant Hydac, Talos Castor, Space Data LCLV, Black Brant XII, HPB, Black Brant XI, Starbird. Propellants: Solid. Stages: Talos Mk 11 Mod 2. Agency: Alleghany, Hercules.

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