Hapith T
PAYLOAD

Feature

The payload fairing of Hapith V is constructed by using lightweight composite honeycomb sandwich structure with ample thermal and environmental protections.

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MATERIALS

Feature

Hapith V is designed to be constructed using mainly lightweight high strength carbon composite flight structure.

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AVIONICS

Feature

TiSPACE avionics and GNC flight control subsystem are developed simultaneously such that their performance can be checked and verified through real time simulations with the enhancement of a high precision rate table testing platform.

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LELIEN

Feature

LELIEN engine is designed based on a high-efficiency N2O/SBR hybrid rocket technology with specially formulated high density and high energy SBR solid grain and N2O injection scheme that gives our propulsion system close to ideal overall thrust performance.

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HAPITH V 
使用頂尖、非爆炸式混合火箭技術的具成本效益的太空發射系統。我們的混合火箭引擎提供了一流的火箭引擎性能，能夠實現快速的太空發射服務。

有效載荷

將微型和小型衛星送入低地球軌道（LEO）和太陽同步軌道（SSO）

HAPITH V 概述

MAX. LEO PAYLOAD MASS
390 KG

MAX. SSO PAYLOAD MASS
350 KG

ALTITUDE
600 – 700 KM

HEIGHT
20 M

DIAMETER
2.2 M

STAGES
3

UPPER STAGE

單一混合火箭引擎，配備有可轉動的推力向量控制（TVC）和冷氣體反應控制系統（RCS）。

THRUST  10KN

SECOND STAGE

四台混合火箭引擎集群，配備可轉動的推力向量控制（TVC）。

THRUST  80KN

FIRST STAGE

五台混合火箭引擎集群，配備液體噴射向量控制（LITVC）

THRUST  650KN

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