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
Advanced Scout
Part of Scout
Advanced Scout
Advanced Scout
Credit: © Mark Wade
American all-solid orbital launch vehicle. Proposed upgrade of Scout proposed by the University of Rome with two strap-ons from the Ariane 4. Launch would have been from Italy's San Marco platform off Kenya. Further work cancelled in 1993.

AKA: Scout 2. Status: Study 1993. Payload: 521 kg (1,148 lb). Thrust: 1,259.30 kN (283,102 lbf). Gross mass: 39,530 kg (87,140 lb). Height: 23.00 m (75.00 ft). Diameter: 1.14 m (3.74 ft). Apogee: 200 km (120 mi).

LEO Payload: 521 kg (1,148 lb) to a 200 km orbit at 1.00 degrees. Flyaway Unit Cost 1985$: 8.000 million.

Stage Data - Advanced Scout



Family: all-solid, orbital launch vehicle. Country: USA. Stages: Ariane 3-0 P7.35, Algol 3, Mage 2, Altair 3, Castor 2. Agency: Vought.
Photo Gallery

Scout 2Scout 2
Credit: ESA



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