In-Orbit Service

Enabling HyImpulse in-orbit capabilities for small satellite missions

SR75 (Suborbital Rocket)

A single-stage, 13m tall rocket utilizing one HyPLOX‑75 hybrid engine to lift up to 200 kg to ~250 km; serves as both a commercial service (microgravity research) and tech demonstrator for SL1.

Our Story

BUILT BY CREATORS, FUELED BY IMPACT

This template was born from a belief that design should lead with strategy. Our team blends brand architects, UX specialists, content experts, and growth minds—all collaborating toward measurable results.
 Every project is a journey shaped by passion and purpose.
 We don’t just adapt to change—we create it.

Meet HyMOVE

Hylmpulse's next-generation Orbital Transfer Vehicle (OTV) designed to provide flexible and efficient in-space transportation services.

About

HyMOVE is a versatile in-space transportation system for small and heavy launchers, enabling efficient satellite deployment and payload hosting. It supports missions such as station-keeping, orbit adjustments, deorbiting, and interplanetary transfers. With a modular, optional hybrid rocket engine using storable oxidizer, HyMOVE offers high thrust, flexibility, and a low-cost, high-performance propulsion solution. Commercial deployment is planned by 2029, making it a key platform for in-space logistics and services.

Characteristics

Payload Capacity: Up to 400 kg
Hybrid Engine: N₂O/HTPB, 4 kN thrust class (combined with N₂O/C₂H₆ bi-propellant thrusters)
Oxidizer Tanks: Type 3 COPV
Core and Thrust Structure: Laminated CFRP
Payload Plate: Composite sandwich panel

Advanced
Orbital Services

Re-entry assistance

Constellation deployment with precision phasing

Multi-payload deployment across multiple orbital planes

Hosted payload services

In-Orbit constellation replacement services

Cold Flow Test

Capacity & Precision

Payload mass: 400kg Payload volume: cylindrical 3m. +-4 km target orbit precision

Longevity

Mission Duration: 2+ years Data Interface: Standard S-Band, RS 422 or Ethernet Available Power: 45 W (orbit averaged), 140 W

Maneuverability

OTV is capable of controlling 6 orbital parameters Fastest time to target orbit: 10 hrs to 2 days