Flight 3

Overview

Destination: Sub-Orbital
Mission: Suborbital

Sub-Orbital Taiki-cho, Hokkaido, Japan Taiki-cho, Hokkaido, Japan

Flight duration : 515 seconds Maximum altitude : 113.4 km Downrange : 37 km from the launch site This was the first successful attempt following two consecutive failures for the previous MOMO series, and has provided valuable telemetry data for further development within IST.

MOMO

Family: MOMO
Configuration:

Momo is a Japanese sounding rocket capable of delivering 20 kg to a height of 100 km. It is privately developed by Interstellar Technologies Inc. (IST). The single stage Momo is powered by a pressure-fed engine fueled with ethanol and liquid oxygen. The engine is gimbaled for steering, with cold gas thrusters providing roll control.

See MOMO Details
Specifications
  • Stages
    1
  • Length
    9.9 m
  • Diameter
    0.502 m
  • Fairing Diameter
  • Launch Mass
    1 T
  • Thrust
    12 kN
Family
  • Name
    MOMO
  • Family
    MOMO
  • Variant
  • Alias
  • Full Name
    MOMO
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Interstellar Technologies

Circle Image
Takahiro Inagawa Founded: 2005 Successes: 1 Failures: 4 Pending: 1

Agency Type: Commercial

Interstellar Technologies, Inc. (Japanese: インターステラテクノロジズ(株) Hepburn: Intāsutera Tekunorojizu (kabu)) is a Japanese NewSpace company. It is a rocket spacelaunch company developing the MOMO launcher. Its stated goal is to reduce the cost of access to space. In 2017, it became the first Japanese company to launch a privately developed space rocket, though the launch was unsuccessful. The company plans to complete a rocket by 2020 that would be capable of launching small satellites into orbit.

INFO WIKI

Taiki-cho, Hokkaido, Japan

Pad: Taiki-cho, Hokkaido, Japan


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