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Illuminated Rock

World's safest and most efficient
GREEN PROPULSION SYSTEM 

I-Booster

At Manastu Space, we are developing the world’s safest and most efficient green propulsion system to replace the highly toxic, carcinogenic and inefficient fuel of the satellite. Manastu has built a novel propellant MS-289 which is a proprietary blend of Hydrogen-peroxide and additives which is combusted by a novel high temperature catalysts to enable this high performance.

Thruster
Higher performance, manastu space

50% Higher Performance

Due to higher combustion temperature and higher density of our fuel and engine design

Manastu Space

>20x More Agile

Agile System due to ability to produce higher thrust compared to Electric Propulsion

Manastu space

Green & Affordable

Fuel is as safe as common salt, hence less safety precuations and less infrastructure cost. 

Green Propulsion System
Technical Specifications
 
(for >100 kg satellites)

Type

Monopropellant

Thrust Class

0.5N, 1N, 10N, 22N

 

Specific Impulse 

>260 s

Total Impulse 

> 10,000 Ns

Propellant mass  

4 kg (with safety margin)

Mass Dry/Wet

6 kg / 10 kg

Density Specific Impulse

>320 s

Dimensions  

600 * 600 * 300 mm

Collision Avoidance System
for Cubesat  

We are working on a dedicated debris collision avoidance system based on a high performance green propulsion system. This system can operate with a primary propulsion system for satellites. One of the major features of this system is operation in short duration. As per the data from Space Situational Awareness system, thrusters are operated with inputs from OBC to reduce the fuel requirement. At the end of the mission life, same system can be used for the deorbiting the satellite.

Vyom 1U Module

1U Vyom
Technical Specifications
(for 5U to 24U+ satellites)

Type

Monopropellant

 

Thrust

0.5N, 1N

Specific Impulse

>250 s

Total Impulse 

> 1200 N-s

Propellant mass  

500 g (with safety margin)

Mass Dry/Wet

900 g / 1400g

Dimensions  

100 * 95 * 95 mm

Vyom 2U Module

Technical Specifications
(for 5U to 24U+ satellites)

Type

Monopropellant

Specific Impulse

>250 s

 

Thrust 

0.5N, 1N

 

Total Impulse 

>2700 N-s

2U Vyom

Propellant mass  

1100 g (with safety margin)

Mass Dry/Wet

1200 g / 2300 g

Dimensions  

200 * 95 * 95 mm

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