Sundancer Orbital Trajectory Implications (Part Three)

Sundancer Orbital Trajectory Implications (Part One)
Sundancer Orbital Trajectory Implications (Part Two)

Henry Spencer was kind enough to send me some feedback on the first two posts in this series, and it appears that I forgot to highlight what both of us see as the key benefit of such repeating ground track orbits: first orbit rendezvous.

First Orbit Rendezvous
Orbital Mechanics isn’t my strongest suit, but I’ll try to explain. For optimal launches you want the destination plane to cross through your launch site. For typical, non-repeating orbits like that of ISS, a given launch window won’t actually have the station itself passing directly overhead, just the plane. So what you do is you launch into what’s called a “phasing orbit”. Basically orbits at different altitudes will complete a revolution in a different amount of time, with lower orbits being faster. So, basically you go around a bunch of times before things actually line up for the transfer out to the final orbit. That’s probably a painfully oversimplified explanation, but gives the general idea.

The problem is that orbit phasing like this typically requires as much as 3 days between launch and rendezvous. That’s a long time. When you think about it, that’s actually about the same time it would take for a vehicle to travel from LEO to a lunar orbital station! Imagine how much fun that must be in something cramped like Soyuz. Long phasing time requirements like that drive up the design complexity and cost of a transfer vehicle, while also typically making it less comfortable. Basically, instead of being just a simple LEO equivalence of a Toyota Corolla, it ends up being an orbital RV, just more cramped.

On the other hand, if both the plane of the station and the station itself cross over the launch site daily, you can do a “first orbit rendezvous”. Ie you don’t have to do phasing orbits first, and could be done with rendezvous and docking in as little as 90 minutes, possibly less with practice. This allows you to go with a much more spartan, lightweight, simple, and inexpensive transfer vehicle. It also makes the trip to orbit a lot shorter, so you get to spend more of your time at an actual station or transfer vehicle which can afford to have nicer…er facilities. Being able to avoid the need for the “diapers” is probably well worth it.

The other nice thing is that once things have gotten going well enough that you have a steady flow of vehicles up and down from the station, the stay-time of any individual vehicle can be kept relatively short, allowing you to turn things around more frequently. This is at least part of the reason why multi-hundred million dollar airplanes can keep costs low enough that Joe Schmoe can buy a ticket from LA to New York for a price that is actually not much more expensive than driving (and possibly cheaper).

Other Repeating Ground Track Orbits
Another thing worth mentioning is that just about every inclination you can imagine has these repeating ground track orbits. It’s just a case of matching things like the time it takes to complete an orbit, and how fast the earth is rotating underneath you. It’s substantially more complicated then that in detail (as usual in engineering), but this 41 degree orbit isn’t the only resonant orbit out there. There exist repeating ground track orbits in 51.6 degrees for instance. I do believe the one which repeats every 24 hours ends up being not much more than 100km higher than ISS is currently located. A friend of mine actually suggested boosting ISS into such an orbit to make it easier to access for multiple users. If ISS weren’t being run partially by NASA (ie if they say auctioned off their stake in things), that might not be a bad approach to things.

[Note: Hopefully sometime next week I’ll have a global ground track to discuss.]

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Jonathan Goff

Jonathan Goff

President/CEO at Altius Space Machines
Jonathan Goff is a space technologist, inventor, and serial space entrepreneur who created the Selenian Boondocks blog. Jon was a co-founder of Masten Space Systems, and is the founder and CEO of Altius Space Machines, a space robotics startup in Broomfield, CO. His family includes his wife, Tiffany, and five boys: Jarom (deceased), Jonathan, James, Peter, and Andrew. Jon has a BS in Manufacturing Engineering (1999) and an MS in Mechanical Engineering (2007) from Brigham Young University, and served an LDS proselytizing mission in Olongapo, Philippines from 2000-2002.
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11 Responses to Sundancer Orbital Trajectory Implications (Part Three)

  1. Rand Simberg says:

    Jon, you might want to provide links to the previous posts in the series so those coming to the permalink can find them easily.

  2. Jon Goff says:

    Good suggestion. How’s that?


  3. Anonymous says:

    Thanks for posting this information, Jon.

    The orbit really makes the job of the crew ferry much easier. Environmental systems can be pretty bare-bones, elminating the need for solar panels or large fuel cells also. Just run off of batteries.

  4. Rand Simberg says:

    Environmental systems can be pretty bare-bones, elminating the need for solar panels or large fuel cells also. Just run off of batteries.

    Not if you want any mission margin. A nominal mission can be one-day, but you have to be prepared for excursions, unless you want to abort back to earth.

  5. Jon Goff says:

    A lot also depends on what infrastructure there is in place. If the station has a tug for instance, that reduces the odds that you’d have to do a surface abort if something goes wrong. But the possibility of keeping environmental controls nice and simple for the orbital craft is definitely appealing.


  6. Ferris Valyn says:


    With the news coming out of Planetspace, do you think that Cape Brenton is a possiblity, or would Planetspace have to open up a second launch site?

  7. Jon Goff says:

    Cape Brenton is too far off the groundtrack. The highest latitude the groundtrack reaches is just north of New York City. Now, if ISS were say boosted up to a resonant orbit, they might be able to launch to that, but otherwise they’d need a lower latitude launch site to reach Bigelow’s station.

    Also, it’d be nice to see more actual real progress from the PlanetSpace/Canadian Arrow guys. They’ve been around longer than we have, probably have a lot more people, and definitely have had more money, but haven’t really had any new progress to talk about in a couple of years–just all sorts of interesting plans for the future.

    I’m not saying that they aren’t doing interesting things, it’s just that until I see signs of actual progress, I am probably going to stay rather skeptical about the whole thing.


  8. adiffer says:

    Orbit nodes and perigee points precess at that inclination. Isn’t that going to slowly mess up the resonance effect?

    As a perturbation I imagine it would shift the repeating ground track over time and leave you having to do the phase trick some of the time from any one launch site.

  9. Big D says:

    How tight is your launch window if you want to dock on the first orbit?

  10. Jon Goff says:

    Big D,
    Not entirely sure. I imagine that for a first orbit rendezvous it’s fairly tight. But that’s just a guess.

  11. Pingback: AAS Paper Review: Practical Methodologies For Low Delta-V Penalty, On-Time Departures To Arbitrary Interplanetary Destinations From A Medium-Inclination Low-Earth Orbit Depot | Selenian Boondocks

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