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Headquarter

Sumitomo Fudosan Hamacho Building 3F, 3-42-3, Nihonbashi Hamacho,
Chuo-ku, Tokyo
Japan 103-0007

DENVER, US

Colorado 12876 E Adam Aircraft Circle, Centennial,
CO 80112, United States
Denver, US

LUXEMBOURG

5 Rue de l’Industrie 1811,
Luxembourg

APEX 1.0
Lunar Lander

OVERVIEW

ispace – U.S.’s APEX lunar lander is a platform vehicle with three configurations – Equatorial, Polar, and Orbital – to enable missions to a variety of landing sites on the lunar surface and to deliver payloads in lunar orbit.

Designed, Manufactured, Assembled, and Launched from the United States

APEX 1.0 Lunar Lander specification

SIZE:
Height approx. 3.3m
Width approx. 4.5m
(Landing legs extended)

WEIGHT:
Approx. 5,390kg（Wet）
Approx. 1,730kg（Dry）

DESIGN Payload Capacity:
Max. 500kg

ABOUT APEX 1.0:
Improved durability, reliability, and manufacturability of the main structure to ensure consistent environmental performance over a wide range of payload carrying areas

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