Friday, August 16, 2013

CYLERS TO MARS: MARSONANCE

Above diagram shows a notional asteroid orbit as it intercepts orbits of Earth and Mars. (Asteroid could be any orbiting object, perhaps a man made, spinning habitat designed to simulate gravity via centrifugal force.)  Above object's orbit has same period as Mars; thus, a fortuitous resonance could enable a habitat to rendezvous with Mars every 1.88 years. This orbit is designed with a perihelion (q, closest point to Sol) of 1.0 AU, radius of Earth's solar orbit.  If habitat adapts this orbit, q is the position to effect a periodic rendezvous for Habitat to exchange pax/cargo with Earth bound enterprises.  Unfortunately, Earth rendezvous opportunities would be rare for above orbit. Since the orbital period (1.88 years) is a multiple of Mars's orbit (1.88) but not Earth's period (1 year), it resonates with Mars but not with Earth.
Consider orbits with Mars's resonance.
 (i.e., "Marsonance", a term coined for this chapter.)
Perihelion
q
Semiminor Axis
b
SemiLatis
Rectum
(AU)(AU)(AU)
0.2
0.75
0.37
0.4
1.03
0.69
0.6
1.21
0.96
0.8
1.34
1.18
1
1.43
1.34
1.2
1.49
1.45
1.4
1.52
1.51
0 < q < a b=(q(2a-q)) = b2 / a
a = 1.52 AU
Focus (c):  c = a - q;
 thus, c2 = a2 -2aq + q2   
Furthermore,
b2 = a2 - c2;
thus, b2 = 2aq - q2  = q (2a - q) 
Semiminor Axis (b):b = (q (2a - q))

Semilatus Rectum(): a: b as b: ℓ;
thus,    = b2 / a
Thought Experiment (TE) assumes an existing asteroid could transform into a habitat,
and orbit could be modified for continuous habitat transfer between planets.
To plan continuous periodic rendezvous between Habitat and Mars,
choose Habitat Period (TH) to equal period of Mars (T)
TH = 1.88 yr = 686.67 days = T
According to Kepler, semimajor axis (a) can be determined from T as shown:
a = ∛(T2) =  ∛(1.882) = 1.52 AU
For any orbit, perihelion (q) can be any nonzero value up to a max of a, semimajor axis.

Thus, "q" can be expressed as percent of semimajor axis (%a) and/or Astro-Units (AU).
q%a = q (AU)
39% a = .6 AU
66% a= 1.0 AU
92% a= 1.4 AU
e(a-q) / a.6050.342.079

Eccentricity (e) quantifies
"flatness" of orbit.
For Habitat orbit q > Earth's orbit (1.0 AU; EXAMPLE: far right), orbit does not intercept Earth orbit;
thus, a habitat cannot use this orbit to transfer from Earth orbit to Mars orbit.
For q = 1.0 AU (middle), Habitat orbit might intercept Earth orbit at q,
but it's very unlikely that Habitat will actually rendezvous with Earth at time of intercept.
For q < 1.0 AU (left), Habitat orbit intercepts Earth orbit at two points;
this increases frequency of actual rendezvous event with Habitat and Earth.
Flatter orbit enables "transfers" between planet orbits.
For simplicity, assume all three orbits to be coplanar; inclination is considered later.

Most Solar objects orbit in a counter clockwise (CCW) direction as observed from north of the Earth.

Most solar objects use a reference ray at orbit's perihelion, q. Thus,  Habitat's angular distance (Θ) is 0° at q, and increases in a CCW direction.

Arbitrarily design Habitat's orbit so  q happens at 40° behind Earth and 69° behind Mars. This arrangement enables Habitat to rendezvous with Earth 51 days after q; 67 days after Earth, it could rendezvous with Mars.

IT TURNS OUT that such a rendezvous would be rare for Earth, because this same configuration would seldom repeat. 

However, orbital resonance enables Habitat to rendezvous with Mars at same position for every orbital cycle.

Selected Orbital Elements
Orbital
Period
Semimajor
Axis 
Semilatus
Rectum 
Semiminor
Axis 
 FocusEccen-
tricity 
Angular
Positions 
ObjectTab ce ΘΘi+1 
Earth (ⴲ)1.00 Yrs1.000 AU 1.00 AU1.000 AU 0.017 AU0.0167TBDTBD
Habitat (H)1.88 Yrs1.523 AU 1.00 AU1.234 AU 0.896 AU0.586
Mars (♂)1.88 Yrs1.523 AU1.51AU1.516 AU0.142 AU0.0933TBDTBD
GivenObserved (T2) b2 ÷ a(×a)√(a2-b2) c ÷ aGiven
Above orbital elements can be observed for Earth and Mars.
TE assumes that humanity will someday deploy a Habitat in an orbit designed for optimal, periodic transport between Earth and Mars.
Thus, Habitat's orbital elements were chosen, including first two angular positions:  Θand  Θ1 .
Angular positions for Earth and Mars are determined in following tables/diagrams.
Habitat velocities range from over 47 kilometers per second (kps) to a low of 12.33 kps.
① At Θ = 0°, diagram shows Habitat's semi-orbit at nearest point to Sol, perihelion (q). This particular semi-orbit has Earth leading habitat by 40.16° and Mars leading by 68.60°.  ② At Θ = 45°, all three objects (Habitat, Earth, Mars) have advanced, but the fast moving Habitat has gained on the other two.  ③  At Θ = 90°, Habitat will cross orbit of Earth, because Habitat's orbit is designed that way.  Diagrams shows a rendezvous with Earth for this particular orbit; unfortunately, Habitat orbit does not resonate with orbit of Earth, and this fortuitous event will be relatively rare.  Fortunately, travelers will use "parking orbits (described later) to complete most transits to/from Earth.   ④ At Θ = 129°, Habitat completes rendezvous with Mars. Since Habitat's orbit is designed with same period (T) as orbit of Mars, Habitat will rendezvous with Mars in same position for subsequent orbits; thus, travelers can count on this Habitat for consistent transport to/fm Mars. ⑤ At Θ = 180°, Habitat's semi-orbit is at farthest point from Sol, perihelion (Q). Mars is far away, and Earth has almost completed a full orbit (almost a year) since the first position on the diagram.
H A B I T A TEarth Mars 
Ang. Pos.RadiusX-CoordY-CoordIncr. Distance Ave. VelocityIncr. TimeAng. Pos.Ang. Pos.
ΘΘi+1 RXYΔdVAve ΔtΘiΘi+1ΘiΘi+1
0.630 AU0.63 AU0.00 AU0.0110 AU = 1,646,197 km47.24 km/sec0.40 day40.16°40.56°68.60°68.81°
45°46°0.707 AU0.50 AU0.50 AU0.0128 AU = 1,916,977 km43.75 km/sec0.51 day59.53°60.03°78.90°79.17°
90°91°1.000 AU0.00 AU1.00 AU0.0204 AU =  3,045,924 km34.26 km/sec1.01 day90.86°91.87°95.56°96.09°
129°130°1.584 AU-1.00 AU1.23 AU0.0339  AU =   5,070,645 km23.183  km/sec2.53 day154.20°156.76°129.23°130.59°
180°181°2.416 AU-2.416 AU0.00 AU0.0422 AU =   6,307,907 km12.33 km/sec5.92 day20.31°26.14°249.44°252.55°
Given
 

1+e×Cosθ  
R × Cos(θ)R × Sin(θ)ΔX = Xi+1 - Xi
ΔY = Yi+1 - Yi
Δd = √[(Δx)2+(Δy)2]

Vi=[μSol(2

Ri
-1

a
)]
VAve= (Vi+Vi+1)/2

Δdkm 

VAve 
×day

86,400sec
GivenΘi
+
ω×Δt
GivenΘi
+
ω×Δt
Radius readily computed from Sol to Habitat; then, translate into 2 Dimensional (X.Y) coordinates.
Pythagorean Theorem helps determine incremental distances between selected pairs of positions.
Determine average velocity for each positional pair; divide distance by VAve for approximate travel times.
 Assume Earth's
angular velocity
ω=360°/365.25 day
ωⴲ  = 0.986°/day
Assume Mars's
angular velocity
ω =360°/686.67day
ω♂  = 0.524°/day
Once each year, Earth bound residents can
observe Sol crossing the First Point of Aries (♈);
 this event is commonly known as the Vernal Equinox 
Throughout each year, date indicates position.  

Design Habitat orbit to have same semimajor axis as orbit of Mars; thus, both share same orbital period (1.88 year) which exceeds Earth's orbital period (1 year).

Thus, Earth will repeat much of its orbit while Mars and Habitat complete their respective orbits.  Thus, using Earth dates to track progress of Habitat can result in ambiguities.  Clarify by labeling Earth positions with both date and year. 

However, positions of Mars/Habitat are not ambiguous; thus, they can be clearly marked with Earth date and days of travel (time since Habitat's perihelion, q).
HABITATEARTHMARS
Ang.
Pos.
Incr.
Time
Cum.
Time
DateAng.
Pos.
RadiusCoordinatesAng.
Pos.
Radius Coordinates
ΘHΔtT Mon-DyΘRXYΘRXY
0.40 day 0.40 day Y-1: Aug 140.16°1.00 AU0.76 AU0.64 AU68.60°1.461 AU0.53 AU1.36 AU
 0.40 day0.81 dayY-1: Aug 140.56°1.00 AU0.76 AU0.65 AU68.81°1.461 AU0.53 AU1.36 AU
 0.40 day1.21 dayY-1: Aug 2 40.96°1.00 AU0.76 AU0.66 AU 69.02°1.461 AU0.52 AU1.36 AU
....................................
129° 2.53  day115.70 dayY-1: Nov 25 154.20°1.00 AU-0.90  AU0.44 AU 129.23°  1.605 AU -1.02 AU1.24 AU
....................................
180° 5.92 day   345.11 dayY-1: Jul 1220.31°1.00 AU   0.94 AU  0.35 AU 249.44°1.562 AU-0.55 AU-1.46 AU
....................................
231°2.56 day   571.84 dayY-2: Feb 24243.78°1.00 AU   -0.44 AU  -0.90 AU8.26°1.383 AU-1.37 AU0.20 AU
....................................
358°0.40 day 685.85 dayY-2:  Jun 18356.15°1.00 AU1.00 AU-0.07 AU68.00°1.459 AU0.55 AU1.35 AU
359° 0.40 day686.25 dayY-2:  Jun 18356.55°1.00 AU1.00 AU-0.06 AU68.21°1.460 AU0.54 AU1.36 AU
360° 0.40 day686.65 dayY-2:  Jun 19 356.94°1.00 AU1.00 AU-0.05 AU 68.42°1.460 AU0.54 AU1.36 AU
Given Prev
Table
ΣΔtiConvert TΘi-1
+
ω×Δt


1+e×Cos(θ)
RCos(θ)RSin(θ)Θi-1
+
ω×Δt

1+e×Cos(θ)
RCos(θ)RSin(θ)
Habitat Orbit Starts
  • Reference Ray (Θ =0°) extends from Sol to q, Habitat's perihelion.
  • For Habitat to rendezvous with Earth and Mars, orbit requires indicated lead angles; thus, when Habitat is at Θ =0°:
    • Earth leads Habitat by about 40°. Since Habitat is closer to Sol and quicker in this part of the orbit, it intercepts Earth in 51 days.
    • Mars leads by approximately 69°.  Habitat intercepts Mars after 116 days since it passes q.
  • Since Habitat orbit has same period as Mars, Mars's lead angle repeats for subsequent orbits.  Unfortunately, lead angle of Earth cannot readily repeat.
Habitat Intercepts
Orbit Twice; Mars Once
1st Intercept: 116 days after q (Θ=0°), Habitat will rendezvous with Mars.
③ Habitat's position at 231 days is Θ=159° after q.
④ Aphelion. 345 days  (Θ=180°) into orbit, Habitat reaches farthest point from Sol, also the orbit's slowest point.
⑤ Habitat's position at459 days ; Θ=201° past q.
⑥ 2nd Intercept: 574 days (Θ=231°), Habitat again intercepts orbit of Mars; however, Mars, the planet, is far away and out of sight.
Future Intercepts
Since Habitat orbit has same period as Mars orbit, Habitat will continue Mars intercepts for future orbits.



These will occur at same angle (129°) and  same travel time (116 days since q).
Consider Earth Intercepts During First Orbit.

Traditionally, q, orbit's perihelion, is an orbit's starting point.

For the first orbit, we arbitrarily start this orbit at August 1, which puts Earth leading Habitat by 40°. Furthermore, we arbitrarily place Mars leading by 69°.

Earth's initial position enables rapid rendezvous with Earth after 51 days of orbit from q.
From Earth, Habitat needs 65 days to travel on to Mars. ALTERNATE SCENARIO: Habitat could launch from Earth when Mars-Earth are in Sep 22 positions.)
Habitat orbital period (686 days)  greatly exceeds period of Earth orbit. Thus, clarity requires Earth positions to label with both date and year.

At Mar 22 (Yr2),  Earth reaches 2nd possible intercept point. This is over a year (476 days) since the Mars rendezvous.
.
Habitat completes an entire orbit in 686 days (Jun 19, Yr2); then, it starts another orbit. Fortunately, Mars once again leads by 69°. Unfortunately, Earth no longer leads by 40°; instead it now lags q by 3°.  Thus, habitat's 2nd orbit will likely not intercept Earth in same way.
Forty-one days later (Apr 28), Habitat reaches same position.  Thus, intercept not accomplished.
Consider Habitat's Subsequent Orbits.

Start 2nd Orbit 686 days after start of first orbit. Earth slips from a lead of 40° to a lag of -3°, but Mars maintains lead of 69°.

51 days later, Habitat intercepts orbit of Earth but not Earth.  Earth arrives at this point 44 days later.

③ 65 days later, Habitat again transits Mars.

Aphelion, orbit's farthest point from Sol is also orbits slowest point.  Positions of Earth/Mars not shown, but be assured they are both far away.

Habitat approaches Earth, coincidental.

⑥  2nd Orbit Ends with Earth slipping another 43° behind.  We observe a trend of Earth increasing its lag of 43° per orbit; thus, we conclude that this orbit will not facilitate constant rendezvous with Earth.


CONCLUSION
For Habitats to routine travel to/from Earth, humanity must complement above "Marsonance" orbit. 
Brainstorm produces following ideas; some will be further considered in subsequent chapters.
1.  Multiple Marsonance orbits; increase odds of Earth proximity during Earth orbit intercepts.
2.  Parking orbits:  for some intercepts, Habitat can launch smaller vessel to "park" in slightly smaller/larger orbit which slowly approaches Earth.
3.  Multiple Earth Resonant orbits (period is multiple of Earth's orbit, 1 year) to increase odds of Mars proximity during Mars orbit intercepts.



VOLUME I: ASTEROIDAL
VOLUME II: INTERPLANETARY
VOLUME III: INTERSTELLAR



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