3.2.19 · D1 · Physics › Orbital Mechanics & Astrodynamics › Hohmann transfer — derivation, minimum energy transfer
Ek orbit ek speed–distance bargain hai: jitna door planet se ho, utna hi dheere jaana padta hai, aur yeh trade fix ho jaati hai jab aap orbit ki size jaante ho. Ek Hohmann transfer bas do circular bargains ko ek single stretched loop se jodta hai, har end par sabse chhota possible "speed change" toll deta hua.
The parent note mein jo bhi hai woh kuch symbols par tikaa hai. Neeche, har ek ko zero se build kiya gaya hai: plain words → picture → yeh topic isko kyun use karta hai. Upar se neeche padho; koi bhi cheez use nahi hogi jab tak woh introduce na ho jaaye.
M — woh mass jise aap orbit karte ho
M beech mein rakhey bade object ki mass hai (Earth, Sun). Ek bhaari bowling ball ko ek stretched rubber sheet par baitha hua socho: woh ek dip banata hai. Baaki sab us dip ke around roll karte hain.
G — gravitational constant
G gravity ke liye nature ka fixed "strength dial" hai, universe mein har jagah same number: G ≈ 6.674 × 1 0 − 11 m 3 kg − 1 s − 2 . Yeh mass ko pull mein convert karta hai.
Inhe bundle kyun karein? Har orbit formula mein G aur M saath chipke huye aate hain, hamesha product GM ke roop mein. Toh hum pair ko ek naam dete hain:
μ (mu) — gravitational parameter
μ = GM
Ek number jo batata hai "yeh particular central body paths ko kitna strongly bend karta hai." Earth ke liye, μ ⊕ = 3.986 × 1 0 5 km 3 / s 2 .
Topic ko isko kyun chahiye: derivation mein har speed aur har burn ek formula hai jisme μ hai. Yeh planet ki gravity describe karne wala single knob hai.
r — centre se distance
r planet ke centre se spacecraft tak ki straight-line distance hai — ground se nahi, centre se. Socho planet ke core se ek string bandhi hui hai; r abhi uski length hai.
"Centre se" kyun? Gravity aise kaam karti hai jaise saari M central point par baithi ho, isliye distances us point tak measure ki jaati hain. Yahi reason hai ki Earth ke around ek "7000 km" orbit (radius ≈ 6371 km) surface se sirf ∼ 629 km upar hai.
Common mistake Altitude ko
r samajhna
Sahi lagta hai: "Main 600 km upar hoon, toh r = 600 ." Fix: r = R planet + altitude . Hamesha centre tak measure karo.
Definition Circular orbit
Ek path jahan r kabhi nahi badlta — constant distance par ek perfect ring. Speed bhi constant hoti hai.
r 1 aur r 2 — inner aur outer circle radii
r 1 = chhote starting circle ka radius. r 2 = bade target circle ka radius. Parent ke example mein r 1 = 7000 km, r 2 = 42164 km.
Ab woh shape jo inhe connect karti hai:
Ek "stretched circle" — ek oval. Jahan ek circle ka ek centre-distance hota hai, ek ellipse ka planet se ek closest point aur ek farthest point hota hai.
Definition Periapsis aur apoapsis
Periapsis = ellipse ka planet ke sabse kareeb point (yahan yeh r 1 par hota hai).
Apoapsis = sabse door wala point (yahan yeh r 2 par hota hai).
Figure dekho: transfer ellipse periapsis par inner circle ko kiss karti hai aur apoapsis par outer circle ko. Woh double-kiss hi poora Hohmann idea hai.
a — semi-major axis
a ek ellipse ka half the longest diameter hai — oval ke centre se uski sabse stretched edge tak ki distance. Ek circle ke liye (ek special, un-stretched ellipse) a = r .
a ke baare mein sabse useful fact: closest aur farthest distances add hokar full long diameter dete hain, jo 2 a hai:
r peri + r apo = 2 a
a orbit ki "size" kyun hai
Same a wali do orbits mein same total energy hoti hai, chahe ek fat oval ho aur ek thin sliver. Isliye a orbit ka "energy fingerprint" hai. Yahi exact reason hai ki transfer ellipse ki size hai
a t = 2 r 1 + r 2
— uska long diameter inner kiss (r 1 ) se outer kiss (r 2 ) tak jaata hai.
v — orbital speed
v woh speed hai jis par spacecraft apne path ke saath move karta hai, km/s mein measure ki jaati hai. Yeh yahan ek magnitude hai — bas "kitni fast," direction alag se handle hoti hai.
Parent mein kaafi saare flavoured v 's use hote hain; yahan poora dictionary hai taaki koi subscript tumhe surprise na kare:
Symbol
Plain words
v c 1
inner circle par speed
v c 2
outer circle par speed
v p
transfer ellipse ke periapsis par speed
v a
transfer ellipse ke apoapsis par speed
(square root) kyun? Square root woh tool hai jo squaring ko undo karta hai. Orbital energy naturally humein v 2 deti hai (kinetic energy v 2 use karti hai), isliye actual speed v recover karne ke liye humein jo energy equation deta hai uska square root lena padta hai.
Yeh Vis-viva equation hai, woh ek law jo v , r , aur a ko saath baandhta hai.
Intuition Ise ek sentence ki tarah padho
r 2 : jitna kareeb ho (chhota r ), utna bada yeh term, isliye utna fast jaate ho — jaise ek comet Sun ke around whip karta hua.
− a 1 : ek fixed "tax" jo sirf orbit ki size a se set hota hai. Ek bigger orbit (bada a ) ka chhota tax hota hai, lekin kisi bhi given r par tum slower bhi shuru karte ho.
Saath mein: paas = fast, door = slow, aur size a poora bargain set karta hai. Derivation mein har burn bas yeh equation hai jo do alag r 's par evaluate ki gayi hai.
Humein sirf v circ nahi, yeh kyun chahiye? Ellipse par, r fly karte waqt change hota hai, lekin v circ sirf tab kaam karta hai jab r = a ho. Vis-viva woh general tool hai jo kisi bhi orbit ke kisi bhi point par v deta hai — dekho Orbital energy & semi-major axis .
Δ v (delta-vee) — speed mein change
Greek letter Δ (delta) ka matlab hai "mein change." Toh Δ v = "engine burn ke dauran speed kitni change hui":
Δ v = v after − v before
Socho speedometer needle ek value se doosri par jump kar rahi hai; Δ v us jump ki size hai.
Yeh currency kyun hai: rocket fuel almost directly Δ v par map hoti hai (rocket equation ke through, dekho Delta-v budget ). Kam Δ v = kam fuel = sasti mission. "Minimum energy transfer" ka matlab sach mein hai minimum total Δ v .
Intuition Hum sirf subtract kyun kar sakte hain (vector-add nahi)
Kyunki Hohmann burns tangent mein kiye jaate hain — naya velocity old wale ke same direction mein point karta hai. Ek hi line par do arrows: change bas unki lengths ka difference hai. Yahi tangent burns choose karne ka fayda hai.
Recall Poora symbol table (right side cover karo)
M ::: mass of the central body
G ::: universal gravitational constant
μ = GM ::: gravitational parameter of the central body
r ::: distance from the planet's centre to the craft
r 1 , r 2 ::: inner / outer circular orbit radii
a ::: semi-major axis = half the ellipse's long diameter = orbit "size"
a t ::: semi-major axis of the transfer ellipse = ( r 1 + r 2 ) /2
v ::: orbital speed (magnitude)
v circ = μ / r ::: speed to hold a circle of radius r
v p , v a ::: speeds at periapsis / apoapsis of the transfer ellipse
Δ v ::: change in speed produced by a burn (our fuel currency)
ε ::: specific orbital energy = 2 1 v 2 − μ / r
π ::: 3.14159..., appears in the transfer-time (half-orbit) formula
v_circ on the two circles
Khud ko test karo — answer zor se bolo, phir reveal karo:
μ kya stand karta hai aur G aur M ko glue kyun karein?μ = GM ; yeh hamesha saath aate hain, isliye ek symbol central body ki gravity strength capture karta hai.
Kya r ground se measure hota hai ya centre se? Planet ke centre se: r = R planet + altitude .
a kya hai ek phrase mein?Half the ellipse's longest diameter — orbit ki "size" aur energy fingerprint.
a t = ( r 1 + r 2 ) /2 kyun hai?r 1 par periapsis plus r 2 par apoapsis long diameter 2 a t ke barabar hai.
Vis-viva state karo aur har term ka matlab batao. v 2 = μ ( 2/ r − 1/ a ) ; 2/ r = paas-hai-fast, − 1/ a = size-set tax.
v circ kya hai aur kab valid hai?μ / r , radius
r ka circle hold karne ki speed — sirf jab
r = a ho.
Δ v kya measure karta hai aur hum ise minimise kyun karte hain?Ek burn se speed jump ki size; yeh fuel par map hoti hai, isliye kam Δ v = sasti mission.
Hohmann burns plain numbers ki tarah kyun add ho sakte hain? Burns tangent hote hain, isliye old aur new velocities collinear hoti hain — magnitudes subtract karo, koi vectors nahi chahiye.