Line 18a3s5 Hilbert–Poincaré Series Space Shuttle Booster Designs WOW SETI

Installation Of Nose Cone/ Forward Skirt Onto Left SRB Segments. (MIX FILE)

Space Shuttle Main Engine (SSME)

Line 18a3s5 Hilbert–Poincaré Series  Space Shuttle Booster Designs WOW SETI

part 126 of 100 videos there are more videos after this one i’ll post all then update the #.
Math Equation Wow Seti 1977 radio signal alien

14/

3/4/4/1/1/1/1/11=0.017
14/0.017=823.5294

Feb 10 2012 719pm est

My thoughts

The search for Hilbert in my wow seti pages brings up line 16 a

Key words here:

Hilbert–Poincaré series

David Hilbert and Henri Poincaré

Infinite

coefficient

See more videos about Hilbert.

Line 16a Stereographic Projection Time Lapse Spherical Plucker Coordinates Euclidean Minkowski WOW SETI

Quatum Field Theory + Axiomatic Formulations of Thermodynamics + Hilbert Spaces + Banach Spaces = Linear Topological Space + Vector Space + Hilbert Series + Infinite?

quote

In mathematics, and in particular in the field of algebra, a Hilbert–Poincaré series (also known under the name Hilbert series), named after David Hilbert and Henri Poincaré, is an adaptation of the notion of dimension to the context of graded algebraic structures (where the dimension of the entire structure is often infinite).

It is a formal power series in one indeterminate, say t, where the coefficient of tn gives the dimension (or rank) of the sub-structure of elements homogeneous of degree n.

It is closely related to the Hilbert polynomial in cases when the latter exists; however, the Hilbert–Poincaré series describes the rank in every degree, while the Hilbert polynomial describes in only in all but finitely many degrees, and therefore provides less information.

In particular the Hilbert–Poincaré series cannot be deduced from the Hilbert polynomial even if the latter exists. In good cases, the Hilbert–Poincaré series can be expressed as a rational function of its argument t.

[edit]Definition
Let K be a field, and let 

 be a N-graded vector space over K, where each subspace Vi of vectors of degree n is finite dimensional. Then the Hilbert–Poincaré series of V is the formal power series

A similar definition can be given for an N-graded R-module over any commutative ring R in which each submodule of elements homogeneous of a fixed degree n is free of finite rank; it suffices to replace the dimension by the rank.

Often the graded vector space or module of which the Hilbert–Poincaré series is considered has additional structure, for instance that of a ring, but the Hilbert–Poincaré series is independent of the multiplicative or other structure.

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this quote stands out

In mathematics, formal power series are a generalization of polynomials as formal objects, where the number of terms is allowed to be infinite

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Feb 10 2012 719 pm est

My thoughts

The search for Hilbert in my wow seti pages brings up line 16 a

Key words here:

 Hilbert–Poincaré series

 David Hilbert and Henri Poincaré

Infinite

coefficient

See more videos about Hilbert.

Line 16a Stereographic Projection Time Lapse Spherical Plucker Coordinates Euclidean Minkowski WOW SETI

Quatum Field Theory + Axiomatic Formulations of Thermodynamics + Hilbert Spaces + Banach Spaces = Linear Topological Space + Vector Space + Hilbert Series + Infinite?

The Space Transportation System (STS) is the formal name of NASA’s Space Shuttle, consisting of an aircraft-like orbiter, two boosters and a huge external tank.

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The Space Transportation System (STS) is the formal name of NASA's Space Shuttle, consisting of an aircraft-like orbiter, two boosters and a huge external tank.

quotes to read
Space Shuttle Era: External Tank and Boosters

The main job of the tank is to hold about 535,000 gallons of super cold liquid hydrogen and liquid oxygen. The lower portion of the tank holds the liquid hydrogen, which is the fuel for the engines.

The second-coldest known chemical, it is stored in the tank at minus 423 degrees Fahrenheit. The upper part of the tank holds liquid oxygen, chilled to minus 297 degrees.

The twin solid rocket boosters are bolted to either side of the tank, with the shuttle itself riding piggyback.

The SRBs hold their own fuel, a mixture of powdered aluminum and a chemical called ammonium perchlorate.

When dry, the combination feels like a pencil eraser. The fuel is the “solid” in the solid rocket booster’s name.

The 15-story-tall boosters work much simpler than liquid-fueled rockets that require complex engines and pumps. They produce nearly 7 million pounds of thrust.

The solid rocket boosters do not ignite until the shuttle’s main engines are up and running. At liftoff, flames shoot down through the inside of the booster to ignite the fuel.

Once ignited, the boosters cannot be turned off. A pair of boosters combines to burn nine tons of fuel every second.

The boosters accelerate the 4.5 million-pound shuttle stack to 3,000 miles per hour and 24 miles high in two minutes. By then, most of the fuel is used up and the boosters fall away, leaving the shuttle’s own main engine’s to reach orbit. The boosters parachuted safely into the ocean where they were recovered and reused on later launches.

After the shuttle engines shut down and the orbiter was on its way, the tank fell away and safely burned up in the atmosphere over the ocean.

NASA’s shuttle fleet performed unprecedented work in orbit during its career, whether deploying spacecraft to distant worlds, setting up the Hubble Space Telescope to view the edge of the universe or building the largest orbiting laboratory in history.

Getting into space to perform that historic work took teamwork with the machinery of a shuttle stack. 

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Solid Rocket Boosters
 
Two solid rocket boosters (SRBs) each generate 12.5 MN of thrust at liftoff, totalling up to 83% of the total thrust needed. After two minutes of flight, the boosters are jettisoned at a height of about 45 km. They separate from the Shuttle, deploy parachutes and fall into the Atlantic Ocean for recovery.

Length: 45.46 m
Diameter: 3.71 m
Empty weight of one booster: 68 000 kg
Gross liftoff weight of one booster: 571 000 kg
Thrust at liftoff of one booster (at sea level): 12.5 MN
Burn time: 124 s

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Space Shuttle Main Engine (SSME)
 
Each Orbiter has three Rocketdyne Block II SSMEs, each with a sea level thrust of 1.752 MN at 104% power.

The total thrust of three engines at liftoff is 5.255 MN.

The engines run on liquid oxygen and liquid hydrogen carried in the External Tank.

The burn time of the engines is 480 seconds. 

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