Johnson Space Center

Flight deck of Lunar Module

Description

Role: Lunar landing

Crew: 2; CDR, LM pilot

Dimensions

Height: 20.9 ft 6.37 m

Diameter: 14 ft 4.27 m

Landing gear span: 29.75 ft 9.07 m

Volume: 235 ft³ 6.65 m³

Masses

Ascent module: 10,024 lb 4,547 kg

Descent module: 22,375 lb 10,149 kg

Total: 32,399 lb 14,696 kg

Rocket engines

LM RCS (N2O4/UDMH) x 16: 100 lbf ea 441 N

Ascent Propulsion System

(N2O4/Aerozine 50) x 1: 3,500 lbf ea 15.6 kN

Descent Propulsion System

(N2O4/Aerozine 50) x 1: 9,982 lbf ea 44.40 kN

Performance

Endurance: 3 days 72 hours

Aposelene: 100 miles 160 km

Periselene: surface surface

Spacecraft delta v: 15,390 ft/s 4,690 m/s

 

Done