How to Ship the World’s Largest Space Telescope 5,800 Miles Across the Ocean
nasa.gov
nasa.gov
(Before anyone starts hollering, I earn my bread and butter in the same language, and that'll be what makes me a millionaire in the unlikely event anything ever does. But on the other hand, somebody's gonna mention it, and I suppose it may as well be me.)
[1] https://www.stsci.edu/~idash/pub/dashevsky0607rcsgso.pdf sections 3.1, 3.5, 4.2ff.
[0]: https://jwst.nasa.gov/content/forScientists/faqScientists.ht... [1]: https://www.researchgate.net/figure/The-crew-segment-of-the-...
> The flight software operates the spacecraft and the science instruments. The on-board scripts will autonomously construct and issue commands, as well as telemetry requests, in real-time to the flight software, to direct the Observatory Subsystems (e.g., Science Instruments, Attitude Control, etc.). The flight software will execute the command sent by the calling on-board script and return telemetry, which will be evaluated in real-time by that on-board script. The calling script will then send status information to a higher-level on-board script, which contains the logic to skip forward in the observing plan in response to certain events (see Section 4.1).
- ISS is 400 km from earth.
- Hubble is 500 km from earth.
- The moon is 384_400 km from earth. It took us 3 days to fly there.
- JWST will be 1_500_000 km from earth. It will take 30 days to fly to its final position.
It is launching on an Ariane 5 rocket which has the launch facilities in French Guiana (for the reason I mentioned above).
Edit: Vandenburg is also even worse from this perspective because in order to launch out over the ocean, you are launching against the rotation of the Earth so you have to overcome that velocity. But Vandenburg is often used for polar orbits where the rocket launches almost due south from Vandenburg over the ocean.
The other significant reason for putting a spaceport further south is the inclination of the orbit (angle of the orbital plane to the equator) is limited by the latitude of the launch site (without a secondary maneuver after launch). So for example if you launch due east (which gives the most advantage of the Earth's rotation) from Cape Canaveral, which is at a latitude of ~28 degrees, you will end up in an orbit with a 28 degree inclination. Launching further North or south you end up with a higher inclination either way. So in order to get an inclination close to equatorial it is easiest to launch closer to the equator. Its a bit hard to visualize but this article has some good explanations [0].
It’s launching on Ariane 5 because it is a very powerful and incredibly reliable rocket that can carry a very large and customized fairing for this very large satellite that needs to go very far.
I have heard "The NASA way" called a gold standard of inefficiency. As they fold up operations; who will take over that mantle of ludicrous largess? Not even Blue Origin can gold plate things "just because it looks better that way".
Huh? They had a variety of launchers to pick from.
> design with no consideration for transport or launch
Again, huh? The folding nature of the JWST is specifically a launch consideration; fitting in the available fairing sizes.
Eh? A variety of launch vehicles were available; they chose the most appropriate one.
A major, if not the principle, reason for NASA to exist is space science, not rocket science. Their satellites, research stations, etc are seriously important work. The rockets are definitely important, but primarily as a way to enable the space research.
This is like saying an airline isn't a true airline because they don't design their own planes. It just doesn't make any sense.
NASA is no longer a space launch company. They service existing missions that were planned/designed/launched when I was kid. This pretty much makes them a legacy. Where's the new?
Good. That was never the point of NASA. If they can contract out the launchers to SpaceX, ULA, etc., they can focus on the scientific aspects. Funding launch platforms via CRS and Commercial Crew was one of NASA's smartest and most cost effective decisions.
> Where's the new?
Quite a bit of it is on Mars actively exploring right now.
NASA has never been a space launch company. Or a company at all, for that matter.
They’re a government administration that always contracted out most design work to private firms, with a mission much broader than space launch.
Its why components are called:
Rocketdyne F-1, Grumman LEM, North American Rockwell CSM, Douglas S-IVB
2012: "The secretive government agency that flies spy satellites has made a stunning gift to NASA: two exquisite telescopes as big and powerful as the Hubble Space Telescope. They’ve never left the ground and are in storage in Rochester, N.Y."
Those were just outdated spares predating Hubble, and apparently more advanced: https://www.washingtonpost.com/national/health-science/nasa-...
But both of those are radio telescopes, so a more fair comparison with JWST would be the sizes of optical/near-infrared/mid-infrared telescopes. The Gran Telescopio Canarias has an 10.4m diameter primary that is made of a number of smaller mirrors. Keck's design is the similar (and came before the GTC), though the primary diameter is slightly smaller at 10m. The Large Binocular Telescope (LBT) has two 8.4m diameter mirrors. All three of these telescopes are capable of observing in the mid-infrared; in principle with higher angular resolution but less stable point spread functions and reduced sensitivity compared to JWST.
The Vera Rubin Observatory mirror is about the same diameter as the LBT's mirrors, but the large secondary and tertiary mirrors reduce the collecting area to be equivalent to that of a ~6.7m mirror.
For anyone else: “ While STTARS has previously transported Webb components to other NASA or partner facilities primarily by air, the team chose to transport Webb by sea to Kourou due to the logistics of landing at the Cayenne Airport in French Guiana. The 40-mile (65-kilometer) route between the airport and the launch site features seven bridges that STTARS would have been too heavy to cross. In addition, the drive from the Port de Pariacabo to Webb’s launch site is relatively short. In comparison, a drive from the Cayenne Airport to the launch site, factoring in STTARS’ slow speeds and other constraints, would have taken about two days.”
Telescope in feet 110x18x15
Antonio AN-225 cargo 142x21x14
Edit: it would fit in a Beluga 124x23x23
As to why they chose that, I have no idea
That's why.
(We also like international cooperation. We build the telescope, ESA chips in with the launcher. Same situation with Orion and the ESA's service module.)
It is way cheaper to correct these things on the planet than with bigger rockets.