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
KSR-3
Korean LOx/Kerosene rocket stage using a pressure-fed engine of indigenous design. First flight 2002.

Status: In development. Thrust: 122.50 kN (27,539 lbf). Gross mass: 5,000 kg (11,000 lb). Unfuelled mass: 700 kg (1,540 lb). Specific impulse: 280 s. Specific impulse sea level: 240 s. Burn time: 95 s. Height: 9.60 m (31.40 ft). Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft).

Subtopics
KSR-III South Korean sounding rocket. Test bed for development of an orbital launch vehicle, powered by the liquid oxygen/kerosene engine planned for the KSLV-I. However flown only once in 2002.
Country: Korea South. Launch Vehicles: KSR-III, KSLV-I 2002, KSLV-II, KSLV-III. Propellants: Lox/Kerosene. Stages: KSR-3.
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