More details on this company's engines & rocket.
1. Their LV will be a fully re-usable medium lift vehicle. Payload capacities of 8 tons (with full reusability), 22 tons (with partial reusability) & 24.8 tons (with stages expended) to 400 km LEO. The rocket will also have GTO & TLI capabilities too.
2. The 80kN RP-1/LOX engine, named "Pegasus", shown before is the upper stage engine. Test campaign for this engine will start on 14th of this month. Hot fire by Nov 14th.
3. For the booster stage they are planning a cluster of 9 RP-1/LOX GG cycle engines, each producing 1.2 MN. 430+ kg/sec flow rate. It will run very high chamber pressures. Exact numbers aren't provided. But the turbopumps had to be qualified for PESO 200 bar & PESO 400 bar standards. So, between 20 to 40 MPa. This engine will be called "Stallion".
4. ISRO's LSPC test stand was available for testing. But that facility was built around the SCE-200 engine & was not compatible for this engine. The had to make their own test stand.
5. the "Stallion" will be unveiled in the last week of December or 1st week of January. Hot fire by March-April.
6. First rocket demonstrator flight will happen in Q4 of 2027 or Q1 of 2028 depending on launch pad availability.
7. It would take them 18-20 launches too hit the USD 500 per kg payload cost. In the 1st year of operational use of this launcher, they are planning to do 3-4 launches with an average payload of 8-14 tons. In the 2nd year they are looking at 8-10 launches.