TE
TechEcho
Home24h TopNewestBestAskShowJobs
GitHubTwitter
Home

TechEcho

A tech news platform built with Next.js, providing global tech news and discussions.

GitHubTwitter

Home

HomeNewestBestAskShowJobs

Resources

HackerNews APIOriginal HackerNewsNext.js

© 2025 TechEcho. All rights reserved.

Rocket Lab's engine has electric turbos and 3D-printed primary components

52 pointsby robszumskiabout 10 years ago

9 comments

patrickyeonabout 10 years ago
Very cool. For people running the numbers about launch costs, there&#x27;s a lot more to it than just $&#x2F;kg. There are very big constants in the cost of a launch (even though SpaceX can get 13150kg&#x2F;61M$, I doubt they&#x27;ll offer 1315kg&#x2F;6.1M$), and having final say in launch timing and what orbit you get is worth a fair bit. For now, it&#x27;s relatively cheap to hitch a ride as a secondary to the ISS (or ISS orbit), but 500km sun-synchronous is not nearly as easy to line up.<p>Comparable prices for small sats: Nanoracks quotes 60,000$&#x2F;1U (usually ~1kg) to the ISS. Interorbital quotes 12,500$&#x2F;kg at a 310km orbit (or 8,000$ to use their 0.75kg tubesat).
DannoHungabout 10 years ago
So... are these guys actually going to be able put up a payload and also is there anything really unique about what they&#x27;re doing? 100kg seems like a pretty small satellite for a $5MM launch, though I must confess my ignorance of such matters for commercial launch systems.
评论 #9401010 未加载
评论 #9400955 未加载
评论 #9401407 未加载
tsuraanabout 10 years ago
I&#x27;m curious, given the stated figures (total thrust, rocket dimensions, payload to certain orbits), is it possible to calculate the specific impulse of this new engine (with the atmo nozzles, I suppose)? I couldn&#x27;t find it on their page, and I&#x27;m not quite well-enough versed in rocketry to even know if there&#x27;s sufficient information to figure it out.
NortySpockabout 10 years ago
Why electric turbopumps (requiring independent power) rather than ones powered by the RP1 propellant?<p>EDIT: RP-1 now, not methane
评论 #9401127 未加载
评论 #9400980 未加载
评论 #9401049 未加载
chinathrowabout 10 years ago
No, it has not &quot;all 3d printed parts&quot;.<p>It has, actual quote &quot;3D printing for all primary components.&quot;<p>Big difference.
评论 #9400879 未加载
ericmsimonsabout 10 years ago
Does anyone know what SpaceX&#x27;s target cost per launch is compared to these guys (4.9M)?<p>Also, I&#x27;d never heard of Rocketlab before but it turns out that they&#x27;re back by Khosla Ventures. Pretty cool.
评论 #9400903 未加载
评论 #9400904 未加载
评论 #9400964 未加载
评论 #9400892 未加载
mrfusionabout 10 years ago
Regarding the pump, why can&#x27;t the fuel just be pressurized and not use a pump?
评论 #9402176 未加载
评论 #9402871 未加载
评论 #9401767 未加载
robertandyabout 10 years ago
Somehow for a product of rocketry class, a video of its CEO talking about just photo selfies and video streaming&#x2F;other solved problems seems downright lame.<p>Talk about the capabilities of the rocket instead! The rocket looks cool though.
评论 #9401816 未加载
评论 #9402412 未加载
morbiusabout 10 years ago
Unless they make their schematics and blueprints open-source, this isn&#x27;t worth my time. Space needs to be fundamentally open, driven by visionaries like Musk and Bolden who care far more about the future of humanity than selling product. The hackneyed &quot;open for business&quot; commentator for the video and the seemingly copious patents they&#x27;ve filed for this vehicle don&#x27;t give me much hope. A far more interesting venture is Copenhagen Suborbitals -- they&#x27;ve lost many key people over the years, but their vision is much more altruistic and deserves much more support than some VC-backed team who decided to apply the startup cash-grab culture to rocketry. (and yes, I do know that&#x27;s an incredibly loaded thing to say on a web forum run by a VC)