Push model using huggingface_hub.

README.md

@@ -10,17 +10,20 @@ tags:
 - text-classification
 - generated_from_setfit_trainer
 widget:
-- text: The thrust produced by a rocket engine is a function of the mass flow rate
-    of the propellant and the velocity of the exhaust gases as they exit the nozzle.
-- text: Advanced energy storage technologies, such as Lithium-Ion batteries, offer
-    higher energy densities and longer life cycles compared to traditional Nickel-Cadmium
-    batteries, making them ideal for long-duration space missions.
-- text: The thermal control subsystem must accommodate both internal heat generated
-    by electronic components and external thermal loads from the space environment.
-- text: The structural integrity of solar panels must be robust enough to withstand
-    the mechanical stresses of launch and the harsh thermal cycles of the space environment.
-- text: The satellite thermal control subsystem (TCS) is crucial for maintaining operational
-    temperatures of all onboard instruments and systems within their specified limits.
+- text: Deep throttling capability, which allows a rocket engine to vary its thrust
+    over a wide range, is essential for applications requiring precise landing maneuvers,
+    such as lunar landers.
+- text: The use of staged combustion cycles, such as the full-flow staged combustion
+    cycle, can enhance the performance of liquid rocket engines by utilizing propellants
+    more efficiently.
+- text: The satellite's power budget, which balances generation, storage, and consumption,
+    is meticulously planned to ensure that all systems remain operational throughout
+    the mission duration.
+- text: The thrust chamber is a critical component where the combustion of propellants
+    occurs, generating high-pressure and high-temperature exhaust gases.
+- text: The electrical generation capability of a satellite is primarily determined
+    by the efficiency and surface area of its photovoltaic cells, which convert incident
+    solar radiation into electrical energy.
 inference: true
 model-index:
 - name: SetFit with BAAI/bge-small-en-v1.5
@@ -66,11 +69,11 @@ The model has been trained using an efficient few-shot learning technique that i
 - **Blogpost:** [SetFit: Efficient Few-Shot Learning Without Prompts](https://huggingface.co/blog/setfit)
 
 ### Model Labels
-| Label           | Examples                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         |
-|:----------------|:-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|
-| Propulsion      | <ul><li>'What are the primary challenges in developing reusable rocket engines, and how do they impact cost and reliability?'</li><li>'In liquid rocket engines, the turbopump plays a vital role in feeding propellants into the combustion chamber at high pressures.'</li><li>'The combustion efficiency of a rocket engine depends on factors like propellant mixture ratio, injector design, and combustion chamber pressure.'</li></ul>                                                                                                                                                                                                                    |
-| Power Subsystem | <ul><li>'The energy conversion efficiency of solar cells is influenced by factors such as temperature, radiation exposure, and the angle of incidence of sunlight, necessitating adaptive control mechanisms.'</li><li>'The electrical generation capability of a satellite is primarily determined by the efficiency and surface area of its photovoltaic cells, which convert incident solar radiation into electrical energy.'</li><li>'Energy distribution within the satellite is managed by a network of bus bars and wiring harnesses, designed to minimize resistive losses and maintain voltage stability across all operational conditions.'</li></ul> |
-| Thermal Control | <ul><li>'How do thermal balance tests validate spacecraft thermal design before launch?'</li><li>'The satellite thermal control subsystem (TCS) is crucial for maintaining operational temperatures of all onboard instruments and systems within their specified limits.'</li><li>'Describe the impact of albedo and infrared emissions from Earth on satellite thermal design.'</li></ul>                                                                                                                                                                                                                                                                      |
+| Label           | Examples                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      |
+|:----------------|:------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|
+| Thermal Control | <ul><li>'The satellite thermal control subsystem (TCS) is crucial for maintaining operational temperatures of all onboard instruments and systems within their specified limits.'</li><li>'Phase change materials (PCMs) are employed in some satellite TCS designs to absorb and release thermal energy, stabilizing temperature fluctuations during orbital transitions.'</li><li>'Describe the process and importance of using computational fluid dynamics (CFD) in analyzing spacecraft thermal environments.'</li></ul>                                                                                                 |
+| Power Subsystem | <ul><li>'Electromagnetic interference (EMI) shielding and grounding techniques are essential in satellite design to prevent power system noise from affecting sensitive communication and navigation subsystems.'</li><li>'The structural integrity of solar panels must be robust enough to withstand the mechanical stresses of launch and the harsh thermal cycles of the space environment.'</li><li>'The integration of maximum power point tracking (MPPT) technology enhances the efficiency of solar arrays by dynamically adjusting the load to match the optimal power output of the photovoltaic cells.'</li></ul> |
+| Propulsion      | <ul><li>'The efficiency of a rocket engine is primarily determined by its specific impulse (Isp), which measures the thrust produced per unit of propellant consumed.'</li><li>'Liquid rocket engines utilize cryogenic fuels and oxidizers, such as liquid hydrogen and liquid oxygen, which require complex storage and handling systems to maintain their extremely low temperatures.'</li><li>"Rocket engines operate on the principle of Newton's Third Law of Motion, where the expulsion of high-speed exhaust gases produces a reaction force that propels the rocket forward."</li></ul>                             |
 
 ## Evaluation
 
@@ -97,7 +100,7 @@ from setfit import SetFitModel
 # Download from the 🤗 Hub
 model = SetFitModel.from_pretrained("patrickfleith/my-awesome-astro-text-classifier")
 # Run inference
-preds = model("The thrust produced by a rocket engine is a function of the mass flow rate of the propellant and the velocity of the exhaust gases as they exit the nozzle.")
+preds = model("The thrust chamber is a critical component where the combustion of propellants occurs, generating high-pressure and high-temperature exhaust gases.")
 ```
 
 <!--
@@ -127,13 +130,13 @@ preds = model("The thrust produced by a rocket engine is a function of the mass
 ## Training Details
 
 ### Training Set Metrics
-| Training set | Min | Median | Max |
-|:-------------|:----|:-------|:----|
-| Word count   | 11  | 22.75  | 30  |
+| Training set | Min | Median  | Max |
+|:-------------|:----|:--------|:----|
+| Word count   | 11  | 23.6176 | 30  |
 
 | Label           | Training Sample Count |
 |:----------------|:----------------------|
-| Propulsion      | 15                    |
+| Propulsion      | 13                    |
 | Thermal Control | 10                    |
 | Power Subsystem | 11                    |
 
@@ -157,12 +160,11 @@ preds = model("The thrust produced by a rocket engine is a function of the mass
 ### Training Results
 | Epoch  | Step | Training Loss | Validation Loss |
 |:------:|:----:|:-------------:|:---------------:|
-| 0.0370 | 1    | 0.2266        | -               |
-| 1.8519 | 50   | 0.021         | -               |
-| 3.7037 | 100  | 0.0051        | -               |
-| 5.5556 | 150  | 0.0032        | -               |
-| 7.4074 | 200  | 0.0026        | -               |
-| 9.2593 | 250  | 0.0023        | -               |
+| 0.0417 | 1    | 0.2181        | -               |
+| 2.0833 | 50   | 0.0145        | -               |
+| 4.1667 | 100  | 0.0047        | -               |
+| 6.25   | 150  | 0.0035        | -               |
+| 8.3333 | 200  | 0.0028        | -               |
 
 ### Framework Versions
 - Python: 3.10.12

model.safetensors

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model_head.pkl

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