SRB

E685701

SRB is a powerful solid-fuel rocket component used to provide major thrust during the initial phase of a spacecraft’s launch.

All labels observed (2)

Label Occurrences
SRB canonical 1
SRB-A 1

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf solid rocket booster ⓘ
advantage high thrust at liftoff ⓘ
long-term storability of propellant ⓘ
relative design simplicity ⓘ
canBe expendable depending on mission ⓘ
reusable depending on design ⓘ
classifiedAs non-throttleable rocket motor ⓘ
designGoal provide initial boost through dense lower atmosphere ⓘ
energySource chemical energy of solid propellant ⓘ
engineeringDiscipline rocket propulsion engineering ⓘ
exhaustDirection through convergent-divergent nozzle ⓘ
hasComponent casing ⓘ
igniter ⓘ
insulation ⓘ
nozzle ⓘ
recovery system ⓘ
solid propellant grain ⓘ
thrust vector control system ⓘ
hasFeature can be used in pairs or multiple units ⓘ
fixed propellant grain geometry ⓘ
high thrust-to-weight ratio ⓘ
simple mechanical design compared to liquid stages ⓘ
ignitionType pyrotechnic ignition ⓘ
limitation limited throttling capability ⓘ
thrust cannot be shut down once ignited ⓘ
located sides of the core launch vehicle ⓘ
massFraction dominated by propellant mass ⓘ
mountedOn launch vehicle ⓘ
operatesDuring first stage of ascent ⓘ
operatesIn lower atmosphere and early ascent regime ⓘ
produces high-temperature exhaust gases ⓘ
provides major thrust during initial launch phase ⓘ
requires careful thermal protection design ⓘ
precise propellant casting and curing ⓘ
role augment core stage thrust ⓘ
safetyConcern reliability of ignition system ⓘ
structural integrity of casing and joints ⓘ
separatesFrom core stage after burnout ⓘ
separationMethod pyrotechnic or mechanical separation systems ⓘ
structuralMaterial high-strength steel or composite materials ⓘ
thrustControl grain geometry shaping thrust profile ⓘ
thrust vectoring via movable nozzle ⓘ
usedBy expendable launch vehicles ⓘ
reusable launch systems ⓘ
usedFor overcoming gravitational and aerodynamic drag at liftoff ⓘ
spacecraft launch ⓘ
usedIn multi-stage launch vehicle configurations ⓘ
usesPropellantType solid rocket propellant ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

H-2B → solidBoosterType → SRB-A ⓘ
linked to: SRB