HANBIT-Micro (Equipment) ( 4 )

Description

HANBIT-Micro is a two-stage space launch vehicle, including a kick stage, capable of carrying a 170kg payload to a 500km Sun-Synchronous Orbit (SSO). The first stage of HANBIT-Micro is powered by a 25-ton thrust hybrid engine, while the second stage employs two 3-ton thrust engines, along with the kick stage.

The kick stage enables precise delivery of customer satellites or payloads into their intended orbits, ensuring optimal positioning and maximizing the efficiency and flexibility of space missions.

Thesaurus

rdfs:label : HANBIT-Micro

Browsing

produced by this Company Innospace

produced in this Country Korea

has Keyword small_sat_launcher

belongs to this Weapon System space-based_system


Specifications

Kick_Stage

Propellant: Methane / LOx

Thrust: 4 kN

Burn Time: 390 sec

Specific Impulse: 350 sec

OVERVIEW

Height: 22.5 m

Orbit: ~ 500 km (SSO)

Diameter: 1.4 m

2nd_Stage

Thrust: 29 kN x 2ea

Burn Time: 250 sec

Propellant: Methane / LOx

Specific Impulse: 350 sec

1st_Stage

Burn Time: 130 sec

Specific Impluse: 292 sec

Thrust: 245 kN

Propellant: Paraffin / LOx


Company Data

Contact Pointinnospace@innospcecom
homepage https://www.innospc.com/main