Skip to main content

Questions tagged [booster]

A booster is a type of rocket used to assist in putting larger payloads into orbit. Use with the [rocket] tag any any other relevant launch vehicle tags

7votes
5answers
3kviews

Why doesn't SpaceX use solid rocket fuel?

I am curious to why SpaceX wouldn't use more efficient solid rocket boosters instead of the liquid booster they currently have for the first stage of their Starships. At first, I thought this was due ...
Alex Abramov's user avatar
4votes
2answers
270views

what are some methods of side booster separation?

Through some research, I got to know about the booster separation motors (BSMs) used on the space shuttle in order to separate the solid rocket boosters (SRBs). However I did not understand if this is ...
Aerospace_Nerd's user avatar
1vote
1answer
149views

Did Relativity's Terran 1 booster survive the fall to the ocean for recovery?

There is no plan to recover the booster of the Terran 1 rocket launched yesterday. Did the booster survive (not necessarily intact) the fall to the ocean and the impact with the surface of the water? ...
Rodo's user avatar
  • 953
4votes
1answer
150views

Would it make sense to compress air around a bell nozzle during booster ascent?

Regarding boosters having one single liquid fuel engine, such as Delta 4 for example. Would some sort of annular aerodynamic device, attached to the skirt and placed around the bell nozzle, help ...
user avatar
4votes
1answer
307views

Does a RTLS (Return To Launch Site) landing deposit more soot on the booster than a drone ship landing?

First, it performs an extra burn (the boostback burn). Does this burn make a credible source of extra soot? Second, sometimes it appears to have flown through the second stage's exhaust plume. Does ...
Starship Remembers Shadow's user avatar
1vote
0answers
109views

SLS Block 2: Original thrust

In older graphics depicting the evolution of the SLS vehicle, it states that the Block 2 upgrade was to produce 11.9 million lbs of thrust. At some point in the last few years, however, this has ...
Andykins 's user avatar
2votes
1answer
224views

Has there ever been a fully-reusable big-dumb-booster design proposed?

I know of fully expendable Big Dumb Boosters, as well as "smart" reuse in systems like NEXUS (all versions) and their contemporaries, what I'm trying to figure out (after hours of sorting ...
AnarchoEngineer's user avatar
6votes
2answers
595views

Thrust to weight of large solid fuel boosters

I have been looking at examples of large solid fuel rocket boosters or first stages used for space launch, such as P80, the Space Shuttle SRB, the various versions of Graphite-Epoxy-Motor, the solid ...
Ögmundur Eiriksson's user avatar
30votes
2answers
5kviews

Why do the walls of a solid rocket booster not glow red hot?

After ignition the walls of the SRB are separated from the "reaction chamber" by solid rocket fuel. But as the burn progresses, more and more fuel is used up and so the isolation from the ...
TrySCE2AUX's user avatar
17votes
1answer
3kviews

What is the difference between the solid fuel Boosters of the Shuttle and Artemis?

The Shuttle boosters had 4 segments and Artemis has 5. What are the differences in total mass, thrust and burn time? Is the thrust profile (thrust over time) the same?
Uwe's user avatar
  • 49.7k
2votes
0answers
84views

Atlas V booster appearance change in flight

In the livestream of the latest Atlas V 541 flight launching the GOES-T satelite I saw that the nosecones of the two visible boosters changed the appearance within a few seconds in the flight. Is this ...
Spaceman-21's user avatar
10votes
1answer
500views

What are the advantages of air lit solid boosters in PSLV XL?

ISRO's PSLV-XL has 6 solid strap on boosters. In a typical flight profile 4 strap on boosters are lit on ground just before liftoff. The remaining two boosters are lift 25 seconds later in air. ...
Ashvin's user avatar
  • 3,072
6votes
1answer
587views

What limits pressure buildup in SRB's?

According to st. Robert's Law, propellant burn rates increase with pressure. When an SRB is ignited, propellant starts to burn, making the pressure rise in the combustion chamber. The flow through the ...
eds1999's user avatar
2votes
1answer
450views

Tradeoffs between axial burning and radial burning of solid propellant boosters?

What are the tradeoffs between axial burning and radial burning of solid propellant rocket motors? How would someone determine which to choose according to the mission requirements? In general has ...
Mukul Hatekar's user avatar
5votes
0answers
122views

What would it take to bring VSS Unity over the Kármán line?

There's been a great deal debate about Virgin Galactic calling 50 miles "space", while most use a 100 km Kármán line definition for the term. VSS Unity has exceeded 89 km altitude on two ...
Adám's user avatar
  • 1,587

153050per page
close