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Record W2373202765

Study on factors affecting the output performances of three-impulse-at-one-spot thruster

2011· article· en· W2373202765 on OpenAlex

Why this work is in the frame

A frame that forgets how it found something cannot be audited. These are the routes that admitted this work.

aboutThe title or abstract carries a Canadian signal from the geographic lexicon.
no affNo Canadian affiliation: this work is invisible to an affiliation-only frame.
No Canadian affiliation. An affiliation-only frame, the usual design, would never have seen this work. It is one of the works that make the case for inverting the frame.

Bibliographic record

Venuenot available
Typearticle
Languageen
FieldEngineering
TopicElectromagnetic Launch and Propulsion Technology
Canadian institutionsnot available
Fundersnot available
KeywordsNozzleImpulse (physics)Specific impulseThrustMechanicsChamber pressureMiniaturizationMaterials scienceAerospace engineeringInternal ballisticsEngineeringMechanical engineeringElectrical engineeringPhysicsClassical mechanics
DOInot available

Abstract

fetched live from OpenAlex

Three-impulse-at-one-spot impulse thruster contains three paralleling igniters,which are ignited by external logic circuit and it combusts in the mutual combustion chamber.High temperature and high pressure gas is produced and the gas spouts out through Laval nozzle so that the ballistic trajectory of missiles or rockets' bodies can be corrected many times.The output performance of thrust is the most important parameter to measure the effects of ballistic trajectory correction and it is showed by impulse thrust,pressure in combustion chamber and total impulse.Factors that affect the output performance of thruster were analyzed and studied from three aspects which are the main charging pressure,sealing film force surface diameter and the throat diameter of Laval nozzle.It was proved through a series of experiments that with the increase of main charging pressure,output performance of thruster improved first and then decreased,therefore 21.3 MPa was chosen.A smaller sealing film force surface diameter could prevent sympathetic ignition effectively,but too small diameter could cause an extra energy loss.Therefore,diameter of 3 mm was suggested.When the throat diameter of Laval nozzle rose up,the output performance of thruster was enhanced,but at the same time all structural mass increased,which conflicted with the miniaturization of ballistic trajectory correcting devices.In addition,the trend of output performance change of thruster with the change of main charging amount was most obvious and stable when the throat diameter set to 4 mm.Hence,4 mm throat diameter of Laval nozzle was proposed.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Observational · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.542
Threshold uncertainty score0.557

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0010.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.045
GPT teacher head0.219
Teacher spread0.173 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it