A Corrected BMI for General Use

PUMA represents a major breakthrough in portable metabolic analysis. It is a rugged, compact device that measures human metabolic function at rest, during exercise, in clinical settings, and in extreme environments. Metabolic measurements are a clinically proven method of monitoring cardiovascular health and fitness levels. The PUMA headgear features NASA-developed sensors that evaluate six key metabolic functions. Specifically, PUMA measures oxygen and carbon dioxide partial pressure in addition to temperature, pressure, airflow, and heart rate. By placing sensors close to the mouth, PUMA can record up to 30 (or more) detailed measurements for each breath. From these measurements, PUMA computes metabolically relevant quantities of oxygen uptake, carbon dioxide output, minute ventilation, respiration rate, and heart rate. With additional software, the device computes heart rhythm, tidal volume, and alveolar and dead-space volumes. A small embedded computer controls and acquires data from all sensors at 10 hertz (Hz), performs calculations, and transmits data wirelessly to a remote computer. The PUMA sensors are low power, stable, and capable of operating in a range of environments, including very high and low pressures as well as high- and low-oxygen environments. This portable device provides real-time measurements that are just as accurate as the large stationary metabolic carts used in hospitals. PUMA can be used not only in clinical settings but also in the extreme/remote environments of space, aviation, underwater, and deep underground. Because it detects real-time dangerous drops in oxygen, it can ensure astronaut cardiovascular health; predict the onset of hypoxia in pilots, divers, and first responders; and advance chronic pulmonary disease monitoring and athletic training.

Structural vibrations frequently need to be damped to prevent damage to a structure. To accomplish this, a standard linear damper or elastomeric-suspended masses are used. The problem associated with a linear damper is the space required for its construction. For example, if the damper's piston is capable of three inches of movement in either direction, the connecting shaft and cylinder each need to be six inches long. Assuming infinitesimally thin walls, connections, and piston head, the linear damper is at least 12 inches long to achieve +/-3 inches of movement. Typical components require 18+ inches of linear space. Further, tuning this type of damper typically involves fluid changes, which can be tedious and messy. Masses suspended by elastomeric connections enable even less range of motion than linear dampers. The NASA invention is for a compact and easily tunable structural vibration damper. The damper includes a rigid base with a slider mass for linear movement. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A rack-and-pinion gear coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement. To achieve +/- 3 inches of movement, this design requires slightly more than six inches of space.

The capacitive micro-gravity fluid mass gauge with spatial regularization is a sensor that can be outfitted to propellant vessels and can provide a determination of the mass of liquid and gas inside the vessel volume with a determinable level of accuracy. The sensor consists of 1) a number of discrete electrodes that are installed to the inner surface of the vessel wall, 2) signal generating, digitizing, signal conditioning, and general support (e.g., power supply) electronics, 3) electrical connections between the electrodes and the electronics, and 4) the algorithm used to turn the set of capacitance measurements (i.e., the capacitance matrix) into a volume fraction. The electronics generate and apply a sinusoid to a single electrode, and then the electronics measure the charge on all other electrodes. Capacitance is simply the charge divided by the voltage. This is repeated for all electrodes, without repeating duplicates. For a vessel with a fixed volume, the volume fraction can be converted to the mass fraction using the Ideal Gas Law so long as the fluid constituents, temperature, and pressure are known.

The Standardized Coarse Azimuth Pointing System is a system for any balloon-borne platform with a suspended payload that was less than 5,500 lbs. It separates the rotation of the gondola and the payload from the balloon. The rotator utilizes GPS and solar sensors for command orientation of the payload. There are solar sensors at the top of the rotator providing a 360-degree view. A guidance, navigation, and control system commands sensors to look at a specific point. For example, sensors can detect the position of the sun. The sensor command is sent through the avionics packages on board to start the motor and turn the shaft until the sensors send feedback that they are at the commanded position. The rotator holds the payload at that position until commanded otherwise. The rotator is designed to have a 5 arc-minute pointing capability, and it has demonstrated a 1.4 arc-minute accuracy. The motor runs on a 28V battery source. The system is designed to be operational in a thermal range of -80 degrees Celsius to +50 degrees Celsius. The system can also accommodate the option of integrating a slip ring with 20 separate channels for power, DSL link, and AART communications. The Standardized Coarse Azimuth Pointing System features a hollow titanium shaft, 3-D printed solar sensor mounts, 3-D printed avionics package mounts, and a custom motor frame mount. The system also utilizes 3-D printed templates to standardize the assembly of both rotators, so that nonuniform match drilling is not a problem.

Structural vibrations frequently need to be damped to prevent damage to a structure or payload. To accomplish this, a standard linear damper or elastomeric-suspended masses are used. The problem associated with a linear damper is the space required for its construction. For example, if the damper's piston is capable of three inches of movement in either direction, the connecting shaft and cylinder each need to be six inches long. Assuming infinitesimally thin walls, connections, and piston head, the linear damper is at least 12 inches long to achieve +/3 inches of movement. Typical components require 18+ inches of linear space. Further, tuning this type of damper typically involves fluid changes, which can be tedious and messy. Masses suspended by elastomeric connections enable even less range of motion than linear dampers. The NASA invention is a compact and self-tunable structural vibration damper. The damper includes a rigid base with a slider mass for linear movement. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A rack-and-pinion gear coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement. To achieve +/- 3 inches of movement, this design requires slightly more than six inches of space.