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Questions tagged [performance]

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1 vote
0 answers
123 views

Does an overexpanded nozzle behave like a suction cup?

It is generally said that, to obtain optimal specific impulse, a nozzle should be just the right size that the exhaust pressure is equal to the ambient pressure. Quoting this answer, a relevant ...
Charles Staats's user avatar
10 votes
3 answers
5k views

Do larger rockets tend to have a better mass ratio due to the square cube law?

Do larger rockets tend to have a better mass ratio due to the square cube law? I mean, larger tanks have a better surface-to-volume ratio, so their weight-to-volume should be improved
Krzysiek's user avatar
  • 153
7 votes
1 answer
988 views

Nitrogen trifluoride as a high density oxidiser

Nitrogen trifluoride (NF3) is a liquid between 66K and 144K and has an incredible density of 1.885 g/cm2. It has a pretty great specific impulse, although combustion temp is a bit high, and AFAIK is ...
R. Hall's user avatar
  • 822
3 votes
0 answers
302 views

Using CEA for monopropellants

CEA (Chemical Equilibrium with Applications) calculates chemical equilibrium compositions and properties of complex mixtures and is the industry standard. Applications include assigned thermodynamic ...
R. Hall's user avatar
  • 822
1 vote
0 answers
42 views

How to calculate combustion temp? [duplicate]

I was reading about a propellant combination using ethanolamine(19.9% propellant fraction w/ 1% Copper Chloride) and 90% HTP(80.1%). I am trying to design a hypothetical engine around the propellant, ...
R. Hall's user avatar
  • 822
3 votes
1 answer
268 views

How Intuitive Machines' engines "crank out unmatched performance in the space domain" allowing "transit of Van Allen belts once, unlike competitors"?

According to https://www.intuitivemachines.com/propulsion LOX/Methane Engines Our LOX/Methane engines are unique for in-space propulsion, in that they offer safety in handling and testing here on the ...
uhoh's user avatar
  • 149k
2 votes
1 answer
290 views

How could Starship "deep space variants" improve payload performance by "orders of magnitude" (Elon Musk)?

Replying to Scott Manley's tweeted table of payload mass for a given geocentric C3, Musk tweeted: We could stretch the Falcon Heavy upper stage & increase this a lot, but FH already covers all ...
uhoh's user avatar
  • 149k
6 votes
0 answers
235 views

What are the various ways that rockets measure the instantaneous thrust of each engine?

@DavidHammen's answer to Engine failure: how to detect? mentions thruster sensors. This intrigued me and so I thought I'd ask about how this is done. Thrust is a critical parameter to know in real ...
uhoh's user avatar
  • 149k
9 votes
3 answers
370 views

Is there a formula for converting a rocket's performance for one orbit to another? E.g. SSO performance to GSO?

If a rocket can take 1,000 kg to SSO at 500 km, is that enough information to determine what its capacity to, say, GTO or GSO would be? If so, how would one calculate it?
user40562's user avatar
4 votes
1 answer
851 views

What were/are the stingiest and most generous vacuum nozzle? (records for the smallest and largest expansion ratios)

Vacuum nozzles are huge compared to their sea-level or atmospheric counterparts, as can be seen by comparing the first stage engines on an Electron or Falcon-9 to their second stages, where a big ...
uhoh's user avatar
  • 149k
8 votes
2 answers
858 views

What happened to tripropellant rockets?

IIRC, tripropellant rockets can deliver superior performance compared to bipropellant rockets (at the cost of added complexity). Now, I know that there is the Li/H/F combo, but it isn't used because ...
xilpex's user avatar
  • 183
3 votes
1 answer
173 views

How can I use the Rocket Equation and Staging for a ballistic flight?

I want to calculate the a) thrust b) mass of fuel c) optimal staging of a rocket, which shall fly up to for example an altitude of 50 km in a ballistic flight trajectory. In school I learned the ...
Lucas's user avatar
  • 31
6 votes
2 answers
1k views

Could HIBEX propellant be used for amateur rockets?

The HIBEX rocket was a precursor to the Sprint missile system deployed briefly back in the 1970s. The rocket was only 18 feet long but had extraordinary performance(an acceleration of 100 G's!). But I ...
Mr X's user avatar
  • 183
2 votes
1 answer
245 views

Can a lighter rocket lift more than a heavier rocket?

Let us consider two launch vehicles - "A" and "B". If "A" has a larger wet mass than "B", does this imply "A" has a higher payload capacity to a particular orbit, from a particular launch site than "B"...
Vishnu's user avatar
  • 3,296
5 votes
2 answers
385 views

Why was Apollo 11 launched in summer?

The question could seems stupid, but I think that best moment to launch a rocket is when temperature is lowest in order to achieve the best performance in a reaction engine. I do not know if there is ...
Miguel Hernández's user avatar

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