LE-5B (original) (raw)

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

LE-5B

LOx/LH2 propellant rocket stage. Lower cost version of H-2 second stage.

Status: In production. Thrust: 137.00 kN (30,798 lbf). Gross mass: 19,600 kg (43,200 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 447 s. Burn time: 534 s. Height: 9.20 m (30.10 ft). Diameter: 4.00 m (13.10 ft). Span: 4.00 m (13.10 ft).

Subtopics

HIMES LOx/LH2 propellant rocket stage. .

LACE stage Liquid Air/LH2 propellant rocket stage. .

LE-5EC LOx/LH2 propellant rocket stage. .

Country: Japan. Engines: LE-5B engine. Launch Vehicles: H-IIA 212, H-IIA 202, H-IIA 2024, H-IIA 2022, H-IIA 204. Propellants: Lox/LH2.

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