Author Topic: Skyroot Aerospace  (Read 76082 times)

Offline FutureSpaceTourist

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Re: Skyroot Aerospace
« Reply #120 on: 02/28/2025 03:56 pm »

Offline FutureSpaceTourist

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Re: Skyroot Aerospace
« Reply #121 on: 03/02/2025 01:47 pm »

Offline FutureSpaceTourist

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Re: Skyroot Aerospace
« Reply #122 on: 04/07/2025 05:27 am »

Offline FutureSpaceTourist

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Re: Skyroot Aerospace
« Reply #123 on: 04/28/2025 05:30 am »

Offline FutureSpaceTourist

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Re: Skyroot Aerospace
« Reply #124 on: 05/02/2025 08:41 am »

Offline sanman

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Re: Skyroot Aerospace
« Reply #125 on: 05/15/2025 11:27 am »
Raman Mini Thruster Flight Qualification — Vikram-1 Pre-flight Update


Offline StraumliBlight

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Re: Skyroot Aerospace
« Reply #126 on: 05/21/2025 08:05 pm »


Quote
Our team just nailed the stage separation test of Vikram-1. The ultra-low shock pneumatic separation system we developed in-house worked like a charm, smoothly separating Stage 2 from Stage 3 — in another boost to our journey to orbit!

Online catdlr

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Re: Skyroot Aerospace
« Reply #127 on: 05/22/2025 05:55 am »
We’re now ISO 9001 & AS9100D certified!



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May 21, 2025
This milestone underscores our steadfast dedication to world-class quality and global aerospace standards at every step of designing, manufacturing, and powering our space vehicles.
It's Tony De La Rosa, ...I don't create this stuff, I just report it.

Online catdlr

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Re: Skyroot Aerospace
« Reply #128 on: 06/06/2025 11:39 am »


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Jun 5, 2025
Our Avionics modules are ready for lift-off! 🚀
The suite of in-house developed modules were tested on every signal path for the minutest glitch. They've now been promoted from the lab bench to launch rail — ready to run Vikram-1 autonomously to orbit!
« Last Edit: 06/06/2025 11:39 am by catdlr »
It's Tony De La Rosa, ...I don't create this stuff, I just report it.

Online catdlr

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Re: Skyroot Aerospace
« Reply #129 on: 06/10/2025 01:58 pm »
It's Tony De La Rosa, ...I don't create this stuff, I just report it.

Offline TheVarun

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Re: Skyroot Aerospace
« Reply #130 on: 06/10/2025 09:50 pm »
Based on all the( successful) testing of systems, what would be a good guesstimate for an actual launch? Or is it hard to tell with the information provided?

 

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