We have successfully created an affordable launch vehicle designed specifically for commercial purposes. By utilizing non-aerospace components whenever feasible, we have effectively minimized costs.Our entire range of rocket designs is centered around the innovative Common Propulsion Module (CPM). Initially envisioned as a compact, self-contained rocket system, the CPM demonstrates its capabilities by delivering a 145 kg payload to an altitude of 310 km in a suborbital flight. To accommodate diverse mission requirements, multiple CPMs are combined using parallel staging.While we explored the potential of cryogenic fuel, we ultimately opted for a combination of hypergolic white fuming nitric acid and Turpentine as the oxidizer and fuel, respectively. This choice ensures simplicity in the CPM's design, as its propellants are hypergolic and pressure-fed. As a result, there is no need for ignition and turbopump systems. This streamlined approach maximizes efficiency while minimizing costs.