Please support my efforts. I just finished a conic sections and orbital mechanics coloring book. I need help with printing costs. Through this Kickstarter you can pre-order a signed coloring book. I look at conic sections, Kepler's laws, Hohmann transfer orbits, the Oberth effect, space tethers, Tsiolkovsky's rocket equation and lots of other space stuff. The coloring book is $5 plus $5 shipping and handling ($10 shipping and handling if you're outside the U.S.).

Kickstarter for this coloring book ends 4:30 a.m. April 13, 2020.

__________________________

The internet is a great resource for isolated students like me without access to university libraries or college classrooms. But often Google will land me on a page over my head. I often see strange and unfamiliar terms.

Years ago I found myself gnashing my teeth and crying "What the heck is

**?!"**

*Vinf*Then, as now, Vinf was a common term appearing on web pages teaching orbital mechanics.

Here is a screen capture from Atomic Rockets, a popular resource for science fiction writers:

(red underlines added by me)

And here's a screen capture from a Wikipedia article on hyperbolic orbits:

(red underlines added by me)

In the Wikipedia article they use the symbol for infinity instead of inf. By now you may have guessed Vinf is short for a

**.***hyperbola's velocity at infinity*
But why would we be interested in something an infinite distance away?

A hyperbola gets closer and closer to a straight lines called asymptotes. And as an object moving along a hyperbolic orbit gets farther from the earth, it's speed gets closer and closer to Vinf. A million kilometers out, the actual speed is so close to Vinf that we might as well call it Vinf. From page 36 of my orbital mechanics coloring book:

Page 36 from my coloring book Conic Sections and Celestial Mechanics

The formula for a hyperbola's velocity can be easily remembered if you picture V

_{hyperbola}as the hypotenuse of a right right triangle with V_{escape}and V_{infinity}as legs:
V

_{escape}^{2}+ V_{infinity}^{2}= V_{hyperbola}^{2}I like to talk about hyperbolas but some people don't see the point. A fellow who calls himself Rune has informed me that transfer orbits aren't hyperbolas.

For most transfer orbits, Rune's right. A Hohmann transfer orbit from Earth to Mars is an ellipse with the sun at a focus:

Planet and asteroid orbits are also ellipses about the sun. So what's the fuss about hyperbolas?

To see let's take a closer look at our Hohmann to Mars:

At one scale we see the path as an ellipse about the sun. But magnify the Hohmann path in earth's neighborhood and we see a hyperbola about the earth.

What is the Vinf and Vesc we use to figure the velocity of this hyperbolic orbit? Let's take another look at our Hohmann ellipse about the sun:

What is the Vinf and Vesc we use to figure the velocity of this hyperbolic orbit? Let's take another look at our Hohmann ellipse about the sun:

The speed at the Hohmann perihelion (closest point to the sun) is about 33 kilometers/second. The earth is moving about 30 kilometers/second. So at perihelion, the Hohmann orbit is moving 3 km/s faster than earth.

At the hyperbola's perigee (closest point to the earth), earth escape velocity is about 11 km/s.

So sqrt (V

Which is about 11.5 km/s.

And how about the Mars hyperbolic orbit?

Speed at the Hohmann ellipse aphelion (furthest point from the sun) is about 2.8 km/s slower than Mars orbit.

At a low periaerion, Mars escape velocity is around 4.8 km/s.

So hyperbola speed at the Mars end of the Hohmann is

sqrt (V

Which is about 5.5 km/s.

Rune as well as illustrious people like Dr. Tom Murphy like to say the delta V from earth C3 = 0 to Mars C3 = 0 is around 6 km/s. Those who know how to patch conics will tell you it's closer to 1.2 km/s.

And to properly patch conics going from planet centric to heliocentric orbits we need to know Vesc and Vinf to find the velocity of planet centered hyperbolas. Since it's important, I'll repeat this:

The formula for a hyperbola's velocity can be easily remembered if you picture V

**This 3 km/s is the**.__Vinf__of the hyperbolic orbit about the earthAt the hyperbola's perigee (closest point to the earth), earth escape velocity is about 11 km/s.

So sqrt (V

_{escape}^{2}+ V_{infinity}^{2}) = sqrt (11^{2}+ 3^{2}) km/s = sqrt (121 + 9) km/sWhich is about 11.5 km/s.

**Only .5 km/s greater than the 11 km/s earth escape velocity**And how about the Mars hyperbolic orbit?

Speed at the Hohmann ellipse aphelion (furthest point from the sun) is about 2.8 km/s slower than Mars orbit.

**This 2.8 km/s is the Vinf of the hyperbolic orbit about Mars.**At a low periaerion, Mars escape velocity is around 4.8 km/s.

So hyperbola speed at the Mars end of the Hohmann is

sqrt (V

_{escape}^{2}+ V_{infinity}^{2}) km/s = sqrt(4.8^{2}+ 2.8^{2}) km/sWhich is about 5.5 km/s.

*Only .7 km/s greater than Mars escape velocity.*Rune as well as illustrious people like Dr. Tom Murphy like to say the delta V from earth C3 = 0 to Mars C3 = 0 is around 6 km/s. Those who know how to patch conics will tell you it's closer to 1.2 km/s.

And to properly patch conics going from planet centric to heliocentric orbits we need to know Vesc and Vinf to find the velocity of planet centered hyperbolas. Since it's important, I'll repeat this:

The formula for a hyperbola's velocity can be easily remembered if you picture V

_{hyperbola}as the hypotenuse of a right right triangle with V_{escape}and V_{infinity}as legs:
V

_{escape}^{2}+ V_{infinity}^{2}= V_{hyperbola}^{2}
## 1 comment:

Thanks for the easily understood explanation.

Bob Clark

Post a Comment