41
votes
Since L2 has no visible marker, how will James Webb's ground control determine its relative position and velocity for station keeping?
So how does JWST identify station keeping corrections?
It doesn't.
While the JWST does know where it is pointing, it does not know where it is in space. It doesn't need to. The JWST Flight Dynamics ...
23
votes
Accepted
Is this what station keeping maneuvers look like, or just glitches in data? (SOHO via Horizons)
You are most likely seeing an artifact of how JPL represents its ephemerides for fast numerical computation.
JPL integrates the equations of motion over time. This inevitably results in mismatches ...
23
votes
Accepted
James Webb telescope; limits to propellant lifetime?
For some background see
this answer to Could JWST stay at L2 "forever"?
this answer to What happens to JWST after it runs out of propellant?.
From the 2nd linked answer (slightly edited):
...
20
votes
Accepted
Are any Earth orbits in continual shadow of the Earth?
There is no orbit around the Earth that remains in permanent shadow. Such an orbit would need to have a period of one year, and that orbit would be too large to fit within the Earth's Hill Sphere, ...
19
votes
Accepted
Could JWST stay at L2 "forever"?
According to Wikipedia, the delta-v requirements to stay at L1 or L2 are about 30-100 m/s per year. That seems quite high, however, more likely is around 5-16 m/s. The sun shield has an area of about ...
13
votes
Accepted
Why are 22N and 440N liquid engines quite common?
As noted by @asdfex, 440N and 22N are convenient round numbers in imperial units: 100 lb-f and 5 lb-f.
The exact thrust values for small spacecraft maneuvering thrusters aren't usually critical to ...
13
votes
James Webb telescope; limits to propellant lifetime?
The telescope trajectory changes direction for halo orbit insertion.
Image source: https://jwst-docs.stsci.edu/jwst-observatory-hardware/jwst-orbit
Such a large change of direction would require a ...
12
votes
Accepted
Could a ball of water stay in orbit?
The ball of water in that picture is in orbit; it's just surrounded by (presumably) the ISS.
But a ball of water like that definitely cannot survive in the vacuum of space. Below a certain pressure, ...
12
votes
Accepted
How frequent are (or will be) JWST station keeping burns at L2?
How frequent are (or will be) JWST station keeping burns at L2?
21 or 42 days
I've heard mention of 'every 21 days' which at first look seems excessive but on second look may not be nuts if very ...
11
votes
Are any Earth orbits in continual shadow of the Earth?
One highly reusable observation is the following: For any plane going through the centre of mass, a satellite must spend some part of its orbit on one side of it if it spend some time on the other ...
10
votes
Why is the US building a Lunar Orbital Platform-Gateway (LOP-G)?
A zillion years ago I was at a meeting where large projects were discussed and attempted to be justified. A slide was shown listing say five reasons why project such-and-such was absolutely vital and ...
9
votes
Accepted
Do operating GPS satellites ever make orbital maneuvers for station-keeping?
Yes, GPS satellites do execute station keeping maneuvers. Primary purpose is to keep them within the desired repeating ground track, which leads to a maneuver every year or so for each satellite. I ...
9
votes
Accepted
Moon orbit station-keeping delta-V budget
Here's a paper on LRO stationkeeping. The fundamental problem is articulated on page 3:
LRO will fly in a mean 50 km mission orbit that, for scientific purposes, would ideally be
a perfectly ...
9
votes
Accepted
What orbit would a space station need to stay in orbit for N years?
tl;dr: Park your ISS-like space station above 700 km and there is a good chance it will only lose 100 m/s in 1,000 years due to atmospheric drag at least (and 2000 km for a million years). However, ...
9
votes
Since L2 has no visible marker, how will James Webb's ground control determine its relative position and velocity for station keeping?
Mathematics.
JWST will use the general techniques of locating itself in space - doppler shift, star trackers etc - same thing deep space probes use. Knowing the Sun position, Earth position and their ...
8
votes
Could JWST stay at L2 "forever"?
This paper by Heiligers et al. explores Earth-moon libration point orbits with the addition of solar sail thrusting. While it is of course not directly translateable to Sun-Earth L2 (JWST) the ...
7
votes
Accepted
How do launch and stationkeeping fuel costs vary with altitude?
Your question is hard to answer because it's the reverse of how things are normally done.
Typically satellite missions are driven first by the orbital and lifetime requirements, which determines the ...
7
votes
Accepted
Will the ISS have electric propulsion to maintain altitude? Is there enough power for it?
the VASIMR test planned by Ad Astra has been cancelled:
On December 8, 2008, Ad Astra signed an agreement with NASA to arrange
the placement and testing of a flight version of the VASIMR, the
VF-200, ...
7
votes
Accepted
How much Delta-V is needed for Orbital Maintenance?
Good question, I’m also interested if someone has a more specific answer to share!
On the following table, you can find the required delta-v per year for different orbits.
And about formula, I'm not ...
7
votes
The design of the halo orbit of the James Webb Space Telescope
Has the JWST halo orbit been chosen from a stable halo "template", and in "broad terms", what were the trade-offs between JWST's scientific mission requirement, orbital life-time ...
6
votes
Why is the US building a Lunar Orbital Platform-Gateway (LOP-G)?
I can maybe answer these questions, as someone that has worked on NextSTEP studies (HAB, PPE) and HLS Architecture and Lander Studies. In general, I thought a lot of the news articles were mostly ...
6
votes
Why is the US building a Lunar Orbital Platform-Gateway (LOP-G)?
Let's examine what Jim Bridenstine, current director of NASA and previous member of the Rocket Racing League (1, 2, 3) says.
NASA Administrator Jim Bridenstine Explains the Lunar Gateway is a ...
6
votes
Accepted
Xenon vs Hydrazine, "Should I Stay or Should I go?" Dawn mission decisions
There is one wheel still operable (at least it was operable the last time they operated it), but Dawn no longer uses it. The third wheel failure was in April of this year (2017 for those reading this ...
6
votes
Halo vs Lissajous orbit: Which station-keeping strategy to select and when?
The main difference between the two is that halo orbits tend to be much larger and are constricted to one plane. There's a NASA tech doc from 1993 comparing the station keeping costs between the two ...
6
votes
Accepted
How did DSCOVR use its ten thrusters for the long burn maneuvers MCC and LOI?
The report 'Resurrected DSCOVR Propulsion System – Challenges and
Lessons Learned' contains a schematic of the propulsion system:
and indicates thruster locations:
thruster 9 and 10 are on the ...
6
votes
Could JWST stay at L2 "forever"?
tl;dr: I think there could be room to do this. However, I don't think a conclusive answer can be had through analyses of magnitudes on envelope-backs. A real answer would only come from even more ...
6
votes
How do stable equilibrium points work in GEO? If all geosynchronous spacecraft suddenly lost stationkeeping, would most "fall into" one or the other?
There is a very nice article about the synchronized variation of the debris motion at GEO, available here.
Authors give an example of the 'well-known GEO stable plane, which is a fixed point of ...
6
votes
The Earth's rotation does change by small amounts; what is done to keep geostationary satellites aligned with ground stations?
The very small changes in the Earth's rotation rate pale in comparison to the much larger perturbations that geosynchronous satellites experience from the Earth's non-uniform gravitational field, ...
5
votes
Accepted
What is the Distinction between DSCOVR's "engines" and "thrusters"?
In this case, the terms are being used interchangeably. DISCOVR has one type of engine, i.e. the MOOG Monarc 5N thruster.
DSCOVR is equipped with ten thrusters that can be used for spacecraft ...
5
votes
Accepted
Spacecraft remaining at station-keeping with respect to the ISS
The case of failed docking of Soyuz MS-14 may fit to constraints of the question. It was in orbit near ISS for 3 days between failed docking attempt and successful attempt. The linked above Wikipedia ...
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