Questions tagged [solid-fuel]
Questions about solid fuels. The rockets that use them, the fuels that are burned, and the vendors that make them.
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Is there a purpose in developing a 5 kg kick stage (Star 5A)?
A follow up to Why does the Star-5A have such a bad mass ratio? A comment left by @RussellBorogove says
...the Star-5A is extremely small, at 4.6kg. At that size, the usual observed scaling ...
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Why does the Star-5A have such a bad mass ratio?
I went over the KSP-RO's Discord research notes and found this PDF about the Star kick motors. The OP wrote that the Star-5A had a mass ratio of 0.493, which seems extremely low from a solid motor ...
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Restartable Solid Rocket Motors Through Expanding Throats?
I recall seeing diagrams on a solid rocket motor that could "blow" itself out through suddenly expanding its nozzle, leading to the propellant no long burning or producing any thrust.
First ...
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How exactly does depressurization work in a solid rocket motor?
How does the extinction process actually work in a solid rocket motor?
Most people initially always read that once a solid rocket fuel is ignited there is no way to actually stop its operation until ...
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Why does this sounding rocket have black sooty exhaust with mach-diamond-like oscillations? Is this unusual?
File footage of a sounding rocket with a dark, non-luminescent, sooty exhaust with mach-diamond-like oscillations is shown in the video 1957-1959 IBM 704 Computer - Vanguard Satellite Program "...
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What is the benefit of an inverted rocket stage?
For example the Chinese rocket Jielong 1 has an inverted 4th (final) stage. So the payload sits between 3rd and 4th stage. When 3rd stage separates it has to do a 180 degree turn before igniting the ...
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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 ...
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What is this black smoke coming from an all solid fueled Epsilon rocket?
I saw a clip of a recent (Nov. 5th, 2021) JAXA Epsilon launch on Instagram (link). Shown differently here in a YouTube video @~0:23s:
It's an entirely solid fueled ...
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Solid metal fuel for nano satellite thrusters
A South African company is developing a solid metal fuel thruster that was initially researched by NASA but was not further developed,
an electric reaction could be used to vaporise solid metal fuel, ...
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Rocket equation with Drag factor
For the
avg Thrust of 2 kN,
burn time = 3.5 s,
burn rate= 1.4,
over the time diff of
dt = 0.1 sec
Isp = 140 sec
Cd for the Ogive nose cone C-section = 0.75
Cross-sec Area of the ogive nose cone = 0....
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Calculating the projectile of rocket using RCS to tilt the flight path
If I have main solid rocket with 800 N Thrust, 9 kg in total and has RCS thrusters 0.5 m from the center mass. Mid flight the RCS with 1 N force is activated for 2 sec. How does it affect the flight ...
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The thrust in the calculation of specific impulse
In calculating the specific impulse using the thrust generated as one of the parameters, do we take the total thrust generated or the average thrust over the period of the burn?
$I_{sp} = \frac{F_{...
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Tilted exhaust gases from the rocket nozzle after sonic boom [closed]
Our solid propellant rocket, on test, produces sonic boom. Right after, the plume of exhaust tilts sideways. This will definitely have a gimbal effect during flight. The propellant chamber has one ...
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Why are my empirical and theoretical value of mass flow rate in solid propellant rockets not similar?
For a rocket of:
fuel mass $m_f$ = 6 kg,
Thrust = 3.1 kN, (vs 4k using reducing catalyst to delay burn time)
total powered burn time, $t_b$ = 3.5 s, (using reducing catalyst vs 1.8 sec)
This ...
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What is the max height I can achieve with my solid prop rocket?
For a rocket of:
mass, $m$ = 25kg,
dry mass $m_f$ = 19 kg,
Thrust = 2.1 KN,
total powered burn time, $t_b$ = 3.5 s,
$I_{sp}$ = 129
I get powered burn height = 549 m and total time to max ht of 5506 ...
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Which burning of Solid Propellant is best axial burning or radial Burning?
Which Burning is Better Axial or Radial of Solid Propellant grain used in Solid Rocket Motors?
How Someone Determines which to choose according to the Mission requirements ?
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What are the temperature constraints on various solid rocket boosters?
What are the temperature constraints on various solid boosters/launchers; what are the lowest and highest temperatures they can tolerate? (One answer per booster/launcher/stage)
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Has there ever been a completely solid fuelled orbital rocket? [duplicate]
Engines and fuel management are very expensive to develop, and for smaller launch providers and space agencies this could prevent them from entering the market. My question is, would the cost savings ...
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Can liquid rocket engines have the same thrust as solid rocket engines?
Take the Vega rocket launcher for example. Its first three stages are solid rocket engines and burn at a relatively short time. If I were to change its first stage into a liquid rocket engine, can ...
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What is the effect of calorific value of fuel on the specific impulse of a rocket engine?
What is the effect of calorific value of a fuel on the specific impulse of a rocket engine? Other things remaining the same, and if it is possible to use both, will the same fuel provide the same ...
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Aerospike with solid fuel
I was scrolling in youtube and I saw this awesome video
and I think, if we put an aerospike nozzle in a sounding rocket,or even a small orbital rocket, as a first stage solid booster, this type of ...
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Could one actually make a grain silo rocket?
Watching the recent SpaceX Starship tests got me to thinking:
Could you actually make a rocket using grain as the propellant?
Image from https://www.teslarati.com/spacex-starship-sn5-second-hop-plans/...
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Could the SS520 be used to return a payload from Mars to Earth?
The Japanese SS520-5 nanosat launcher has a payload of 5kg or so to LEO on an all solid fuel rocket with a total mass of about 2.6 tons. To reach LEO its delta-V totalled over all three stages must be ...
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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 ...
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How is solid rocket fuel sourced?
I know that Orbital ATK builds solid rocket boosters, but where do they get the bulk material from? Is there a single supplier or multiple suppliers of solid rocket fuel or do motor manufacturers ...
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Is there any practical application of trinitramide N(NO2)3 in rocket propellants
In 2010 researchers at the Royal Institute of Technology (KTH) in Sweden announced the discovery of new compound, trinitramide N(NO2)3, which could revolutionize production of solid rocket propellants....
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Are more details about the fatal rocket motor accident at Cape Canaveral in April 1964 available?
The 1966 book The Life and Death of a Satellite by Alfred Bester contains an account of a accidental ignition of a third-stage solid rocket motor in a Delta rocket spin test facility at the Cape which ...
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What are the advantages of solid iodine propellant and how is it used for ion propulsion?
I was reading about different sources of propellant for ion thrusters, Xenon being the most common. However, in more recent articles I've found more and more mentions of Solid Iodine being used as ion ...
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Are solid-fueled launch vehicles faster to orbit than liquid-fueled ones?
The (relatively) new Kuaizhou family of launch vehicles is described as "quick-reaction", and is based on ASAT and ICBM heritage.
Solid-fueled rockets have been, historically, cheaper to launch on, ...
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Does this Soyuz vehicle burn coal or oil? What is its official name?
This tweet shows the image below and says:
Soyuz rocket on its way to the launch pad (on a train of course).
Question: Does this Soyuz vehicle (a train engine) burn coal or oil? Does it have an ...
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Was there a history of segmented solid rockets prior to the Shuttle?
The Shuttle famously (perhaps infamously) had its solid rocket boosters built in segments, which were transported to KSC and then joined together. The SLS will similarly have segmented SRBs.
Were ...
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What is the requirement of spacer rings in solid rocket motors in sounding rockets?
I saw this report SOLID ROCKET MOTOR DESIGN L-CLASS, here as shown in FIGURE-8, they have charged the motor with grain segments with spacer rings in between. Can`t we charge the motor without any ...
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Why did the nozzles on the SRB's igniter initiator point toward the grain of the main igniter while the main igniter's nozzle pointed straight down?
How did the shuttle designers make those decisions? What made it a better decision to point the exhaust of the igniter initiator toward the main igniter's grain at an angle? What made it a better ...
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Why doesn't Rocket Lab use a solid stage?
I was just reading about the Scout, an all-solid rocket, and thought of Rocket Lab's Electron, which seems to have a similar mission of deploying small payloads to orbit. I understand the engines to ...
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Which rockets use(d) solid-fuel upper stages?
The Antares is unusual in that it's using solid-fuel in the second stage. I was surprised about that and a couple of questions immediately popped up which are already covered on this site: How can a ...
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How do HMX-fuelled rockets launch without exploding?
Unlike most civilian solid-fuel rockets, which use ammonium perchlorate/aluminium fuels with a rubber binder (known in the industry as ammonium perchlorate composite propellant, or APCP for short), ...
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Solid hydrogen hybrid motor engine for launch?
Would hydrogen unlike water in a solid state take less space or be more stable? How would a rocket work using a block of melting solid hydrogen instead of liquid hydrogen? Has and could any kind of ...
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How do you avoid wasting oxidizer when designing a hybrid rocket?
I was thinking of designing a very simple and small Paraffin rocket engine as an experiment. One thing that I don't understand about these designs is how you efficiently use your oxidizer without a ...
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How much would mass-production impact the cost of solid-fuel rockets?
Let's imagine that, for some arbitrary reason, solid-fuel rocket stages were needed and built en masse in factories, like planes or even like cars.
How much would it drive down the cost of an ...
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Why were large solid-fuel rockets so rare in the past?
When the Germans projected the A4 missile, they discarded solid-fuel propulsion and went on to circumvent the enormous technical difficulties of building a liquid-fuel engine from scratch. Germany had,...
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Have there been any spacecraft with internal SRM other than CONTOUR?
I read about the CONTOUR mission which used an internal solid rocket motor to change the trajectory. Have there been other spacecraft using a solid rocket motor which is not jettisoned after usage?
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Why aren't airbreathing SRBs a thing?
To the best of my knowledge, all solid rocket boosters so far use a propellant that is a solid mixture of both the fuel and the oxidiser parts of the reaction. However, given that SRBs are generally ...
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How far have autophage rockets been developed?
Ars Technica reports on a May 24 phys.org press release/precis on a University of Glasgow paper in Journal of Spacecraft of Rockets about a solid rocket intended to consume itself during use rather ...
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Do launchers using only solid propellant exist?
The question is restricted to launchers that have already been used to launch an object into orbit before today (April 2018).
Some military ballistic missiles run only on solid propergol (e.g. the ...
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Which solid fuel is optimal for light rocket?
I am in search of comparatively cheap and powerful enough solid fuel. I've found rocket candy, but is it enough to reach 1km altitude?
(My aim is a 2 metre high rocket with 0.5kg of payload.)
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Why did Virgin Galactic switch back to HTPB after one launch using thermoplastic polyamide (i.e. nylon)?
A subsection of Second-generation engine in Wikipedia's article on RocketMotorTwo says:
New fuel formulation
Rather than use rubber-based HTPB in the solid portion of the hybrid rocket motor—which ...
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Do the solid rocket boosters of the Shuttle and SLS have a self-destruct system and was it activated during the Challenger disaster?
Videos of the Challenger shuttle explosion show both solid boosters speeding on after the main tank detonated. Were they eventually self-destructed by the ground control, or why not, and why not ...
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How were the Space Shuttle SRBs ignited? (with what?)
I'm unable to find how exactly the Space Shuttle's SRBs were ignited, or what exactly was used to ignite the rocket.
I'm trying to figure out the best way to instantly ignite a solid rocket reliably,...
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How does a solid propellant in a rocket work?
I'm a bit confused about how the fuel manages to get from wherever its being stored in a spacecraft into the engines, seeing as it is supposedly solid and so seems like it wouldn't be easy to move. ...
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Why was the Minotaur V built as a 5-stage design?
Why is Orbital Science's Minotaur V rocket a five stage design? I am aware this is derived from an ICBM design, but why would anyone want a five stage design for launching non-lethal payloads? It ...
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