Where will they launch from?.
Navier is alive 🔥🔥🔥 full video :
This thread should be in the European section no?
I don't think there's a topic for this new French rocket start-up, Venture Orbital Systems. https://www.venture-orbital.comTwitter: https://twitter.com/Venture_Orbital/Their COO has put out an AMA today:https://twitter.com/Venture_Orbital/status/1405797822746828801?s=20
Name change here is their new webpage link. https://www.latitude.eu/100kg to LEO. 9+1 RP1/LOX engine configuration. Nothing about engine type or thrust.
Latitude announced on 22 January that it had closed a $30 million (€27.5 million) Series B funding round to support the development of its Zephyr launch vehicle.
Over the next years, #Zephyr will elevate its #payload capacity, allowed by the technical, industrial and commercial feedbacks and development we gathered in 2023. To follow-up, we upgraded the design of the #Navier #RocketEngine flight version 🎯🚀 Want to dig into the details? A thread 🧵👇
To increase the #thrust delivered by Naviers ⬇️🔥⬇️ our #propulsion team has decided to review the engine cycle to switch from #MotorPump (MP) using batteries to a #TurboPump (TP) using gaz 💪 So, why did we make that choice?
Theoretically, the best developing tech such as a Lithium (Li) & Sulfur (S) battery mounted on an MP stores less energy than High concentration Hydrogen Peroxide (HTP) used on our TP ⚡ Choosing the later technology allows us to optimize the weight/energy ratio 💪 But why use HTP to power it?
An HTP-based TP allows to increase the #shaft power needed for more powerful Naviers and is an easier to handle technology than MP or staged combustion 🙌 Also, the simplicity of this technology fits within our simple design development philosophy: #TheSimplerTheBetter ✅
Furthermore, we gained more advantages by increasing the thrust delivered by each Navier engine! Indeed, single more powerful engines means less engines are needed to meet the overall #performance offered by Zephyr. We are going down to 7 Navier engines to propell the first stage, instead of 9
Within this configuration, each flight Navier on the first stage will deliver 45 kN of thrust in #vaccum conditions and the second stage single Navier will deliver 35 kN of thrust in vacuum conditions 🔝
As for the #alloy used to print the combustion chamber of these flight Naviers, we will be using #Inconel718 as it met our expectations with the test engine: it offers the right thermomechanical properties ✅ Now, you may wonder how is this going to be developed?
Our TP has been designed by our propulsion departement in partnership with @CNES #manufacturers & #labs for quite some time now 👨💻⚙️ And a series of #TestsCampaigns will take place early 2024 using a test bench we designed and installed on our Titan #ResearchCenter on the @AeroParisVatry
These are exciting times at Latitude! 🎉 Have burning questions or eager to learn more? Drop your #queries below! In the meantime, wishing you a Happy New Year filled with joy, success, and endless possibilities! 🌟✨ May the coming year be your best one yet! 🥳