Shuru karne se pehle, yahan poora symbol legend hai aur woh do relations jinpar sab kuch tika hai.
Recall Pressure budget (agar rusty ho toh open karo)
Flow sirf high pressure se low pressure ki taraf jaata hai, isliye tank ko har downstream loss "pehle se pay" karni padti hai. Hydrostatic/acceleration head include karte hue:
ptank=pc+Δpinj+Δpfeed+Δpcool−ρghSign convention:h>0 ka matlab hai liquid surface injector ke upar hai, toh uska weight (ya thrust-acceleration column) liquid ko neeche push karne mein madad karta hai — isliye minus sign, yeh woh pressure kam karta hai jo gas ko supply karna padta. Coasting (g→0) ya bahut chhota column is term ko negligible bana deta hai.
Recall
ptank≈1.5pc kyun (loss breakdown)
Extra half-chamber-pressure ek typical losses ka sum hai, koi magic number nahi:
Injector drop Δpinj≈0.25pc — sabse bada chunk, atomization ke liye zaroori.
Feed-line friction Δpfeed≈0.1pc.
Cooling-jacket friction Δpcool≈0.15pc.
Jod kar: ptank≈pc(1+0.25+0.1+0.15)=1.5pc. Alag-alag designs 1.3–1.5 range mein kahin bhi land karti hain, depending on how these split.
Recall Tank wall mass (corrected derivation)
Hoop stress se thin sphere par, σ=2tpr⇒t=2σpr.
Wall mass = (density)(surface area)(thickness):
mtank=ρm(4πr2)(2σpr)=2σρmp(4πr3)=2σ3ρmpVV=34πr3⇒4πr3=3V use karte hue. Toh mtank=2σ3ρmpV — mass seedha pressure ke saath step mein badhta hai.
Pressure-fed engine mein bilkul koi moving parts nahi hote.
False — isme phir bhi valves aur ek pressure regulator (ek moving element) hota hai. "No turbopumps" hi asli defining feature hai, "zero moving parts" nahi.
Agar tank pressure, chamber pressure ke barabar ho, toh propellant phir bhi dheere-dheere trickle karta rahega.
False — equal pressures par driving pressure difference zero hota hai, isliye mass flow → 0 aur injector atomize nahi kar sakta; engine effectively dead ho jaata hai.
Injector pressure drop wasted energy hai jise designer ko khatam karne ki koshish karni chahiye.
False — yeh ek deliberate, zaroori loss hai: yeh restriction hi liquid ko fine droplets mein todta hai achhi atomization ke liye. Ise khatam karo toh combustion quality khatam.
Chamber pressure double karne se required tank wall mass bhi roughly double ho jaata hai.
True — tank mass ∝p aur ptank≈1.5pc, isliye pc double karne se ptank roughly double hota hai aur hence wall mass bhi, fixed volume ke liye.
Helium isliye choose kiya jaata hai kyunki woh sasta hai.
False — ise isliye choose kiya jaata hai kyunki yeh inert aur light hai: yeh propellants ke saath react, condense, ya dissolve nahi karega, aur low molar mass ka matlab hai given number of moles ke liye kam pressurant mass.
Pressure-fed cycles hamesha zyada reliable hote hain, isliye woh har rocket ke liye best choice hain.
False — reliability real hai, lekin tank-mass penalty (∝p) inhe high-pc boosters ke liye impractical banata hai; yeh sirf wahan jeette hain jahan pc low ho, yaani upper stages.
Ek pressure-fed stage ko complex pump-fed se zyada aasaani se restart kiya ja sakta hai.
True — almost koi moving machinery spin up ya prime karne ke liye nahi, isliye lambi coast ke baad valves reopen karna bahut simpler hai, yahi reason hai ki upper stages ise prefer karte hain.
Pressurant gas chamber mein burn hota hai aur thrust mein add hota hai.
False — yeh design se inert hota hai; iska kaam sirf liquid push karna hai. Yeh combustion mein negligibly contribute karta hai aur aksar specifically isliye choose kiya jaata hai taaki yeh react na kare.
Jaise pressurant emptying tank ko fill karne ke liye expand hota hai, uska temperature constant rehta hai.
False — real expansion adiabatic ke zyada karib hoti hai: gas kaam karte waqt expand karke cool hota hai, isliye uska pressure ek isothermal estimate se zyada tezi se drop karta hai, matlab tumhe simple n=pV/RT figure se zyada pressurant carry karna padega.
"Vehicle ko halka karne ke liye, thin tanks use karo aur compensate karne ke liye sirf pressurant pressure badha do."
Ulta hai — t=pr/2σ se, zyada pressure thicker walls demand karta hai, thinner nahi. High pressure par thin walls burst ho jaati hain; tum inhe freely ek ke liye doosra trade nahi kar sakte.
"Kyunki ptank=pc+losses, zyada bada injector drop use karne se tank halka hoga."
Wrong sign — zyada bada injector drop required ptank ko badhata hai, jo wall mass badhata hai. Yeh atomization improve karta hai lekin tank mass ka cost lagta hai; yeh tank ko kabhi halka nahi karta.
"Bernoulli kehta hai tez flow ka matlab zyada pressure hai, isliye feed line mein propellant ko speed up karna uska pressure chamber mein badha deta hai."
Bernoulli pressure term ke liye ulta kehta hai: zyada speed pressure neeche trade karta hai (21ρv2 badhta hai jaise p girta hai). Feed speed-up pressure head consume karta hai, create nahi karta.
"Tank mass formula m=2σ3ρmpV dikhata hai ki chhota tank (small V) hamesha halka hota hai, isliye tank shrink karo."
V shrink karna tank mass shrink karta hai lekin propellant carried bhi shrink karta hai; rocket equation ke by, kam propellant ka matlab kam delta-v. Tum V freely nahi kaat sakte.
"Regulator ki zaroorat nahi — sirf bottle ko feed pressure par fill karo aur ho gaya."
Stored bottle bahut high pressure par hai aur gas nikalne ke saath uska pressure girta hai; regulator ke bina feed pressure puri burn mein sag kar jaata, engine ko starve kar deta. Regulator ise steady rakhta hai.
"Kyunki gas emptied tank volume fill karne ke liye expand hoti hai, tumhe sirf utna helium chahiye jo final volume fill kare."
Tumhe woh gas bhi chahiye jo storage bottle mein peeche rehti hai (woh kabhi completely empty nahi ho sakti) aur adiabatic cooling ke liye margin, isliye real designs fill-volume estimate se kayi guna zyada carry karti hain.
"Tum tank pressure seedha pc tak gira sakte ho jab tak average feed pressure theek ho."
Cavitation ko ignore karta hai — low feed pressure par liquid locally apni vapour pressure se neeche ja sakta hai, bubbles mein boil ho sakta hai, aur flow choke kar sakta hai; tank pressure ko poori feed line ko vapour pressure se comfortably upar rakhna chahiye.
Propellant ko chamber ke pushback se zyada zyada kyun push karna padta hai?
Kyunki burning chamber gases warna injector ke through backward flow karenge; ek net inward pressure difference hi propellant ko andar move karta rehta hai aur flame ko back up hone se rokta hai.
Low chamber pressure, pressure-fed penalty ko chhota kyun banata hai?
Penalty heavy tanks hai, aur mtank∝ptank≈1.5pc; low pc par woh mass modest hai, isliye simplicity almost free hai.
Same cycle ek sea-level first stage ke liye terrible idea kyun hai?
Boosters high thrust ke liye pc∼100+ bar chahte hain, isliye tanks ko ∼150 bar hold karna padega — wall mass (∝p) prohibitive ho jaata hai, unlike ek pump-fed design jo tanks ko near-empty pressure par rakhta hai.
Hoop-stress balance σ=pr/2t mein 2 ka factor kyun deta hai?
Sphere kaato: pressure halves ko πr2 area par alag push karta hai, lekin resist karne wali wall ring ka area 2πrt hai; "2" us ring circumference se aata hai, isliye pπr2=σ2πrt.
Cryogenic propellants ke liye self-pressurization helium ki jagah kyun nahi le sakta?
Cryogens ki vapour pressure low hoti hai aur self-pressurize karne ke liye huge, cold volumes chahiye; ek inert stored gas controllable, non-condensing pressure deta hai jo propellant ka apna vapour nahi de sakta.
Ideal gas law pressurant size karte waqt enter kyun hoti hai, liquid nahi?
Pressurant ek gas hai jo known volume ko known pressure aur temperature par fill karta hai, isliye n=pV/RT uske moles predict karta hai; liquid propellant incompressible treat hota hai aur woh relation follow nahi karta.
Real pressurant requirement isothermal n=pV/RT estimate se zyada kyun hoti hai?
Expansion almost adiabatic hoti hai, isliye gas kaam karte waqt cool aur pressure lose karta hai; ptank up rakhne ke liye tumhe constant-temperature figure se zyada extra warm gas supply karni padti hai.
Agar vehicle coasting kar raha ho (zero acceleration), toh required tank pressure ka kya hoga?
g→0 hone par head term ρgh vanish ho jaata hai, isliye woh drop out ho jaata hai; tank ko phir bhi pc plus injector aur feed losses chahiye, sirf ±head contribution ke bina.
High acceleration ke under tanks chamber ke upar hone par (h>0), kya liquid weight feed mein help karta hai ya hurt karta hai?
Yeh help karta hai — accelerating column propellant ko chamber ki taraf push karne mein head add karta hai, pressurant ko supply karne wale pressure se ρgh subtract karta hai (budget mein −ρgh term).
Zero feed, cooling, injector losses aur zero head ki ideal limit mein ptank kya hoga?
Yeh exactly pc par collapse ho jaata hai — lekin yeh practically unreachable hai, kyunki zero injector drop ka matlab no atomization aur thus no usable combustion.
Jaise tank drain hota hai aur gas expand hoti hai, gas cooling ke bawajood feed pressure constant kya rakhta hai?
Regulator high-pressure bottle se aur (relatively warm) gas admit karta hai jo emptied volume aur adiabatic cooling se lost pressure dono ko backfill karta hai, ptank steady rakhta hai jab tak bottle mein margin hai.
Pressurant bottle kitni chhoti ho sakti hai, yeh kya limit karta hai?
Ise poore drained volume ke liye enough gas supply karni hai, plus adiabatic-cooling margin, plus burnout par khud ko regulator pressure se upar rakhna; bahut chhoti bottle regulation ke neeche drop ho jaati hai aur feed pressure mid-burn sag karta hai.
Lowest usable tank pressure kya set karta hai, loss budget se independent?
Cavitation — feed-line pressure ko har jagah propellant ki vapour pressure se upar rehna chahiye, warna liquid bubbles mein boil hota hai aur flow choke hota hai; yeh ptank ko floor karta hai even agar nominal losses chhote hain.
Agar ek designer pressure-fed engine se higher thrust chahta ho, toh physically kya constraint karta hai?
Higher thrust ko higher pc chahiye (dekho chamber pressure and thrust), jo higher ptank aur heavier tanks force karta hai — mass penalty hi hard ceiling hai, plumbing nahi.