长寿命原位太阳系探测器(LLISSE)的首次迭代通信电路

J. Jordan, G. Ponchak, P. Neudeck, D. Spry
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引用次数: 2

摘要

金星长寿命原位太阳系探测器(LLISSE)着陆器的第一次迭代通信系统电路是使用美国宇航局格伦研究中心的SiC JFET技术开发的。金星的大气环境恶劣,温度高达460°C,压力1344 psi,由CO2, N2, SO2, HF, HCl, CO, OCS, H2S和H2O组成的致密腐蚀性大气使金星成为电子产品的挑战环境。以前的金星任务持续不到两个小时,但LLISSE正在计划和开发中,可以存活60个地球日。通信电路是在Keysight Advance Design Systems (ADS)中设计的,使用三级差分放大器,偏置电路被设计为开启和关闭开关键控(OOK)调制。电路中集成了缓冲放大器,以方便测试。基于美国宇航局格伦研究中心开发的JFET SiC技术,其设计在室温下工作频率为5 MHz,在460°C时工作频率为2 MHz。OOK具有低功耗的优点,是低频传输的理想选择。SiC JFET已被证明在模拟金星环境中可以存活60天。这些电路在实验室的高温探测站上进行了测试。所述模具安装在用于探测的氧化铝载体上并通过焊丝粘合。两个输出端口提供正负摆动信号,为天线提供平衡信号;输入端口用于偏置和来自传感器数字输出的控制信号。振荡频率、输出功率、相位噪声和数据速率作为温度的函数进行测量。输出功率和相位噪声显示为频率的函数。在室温和金星温度下测量不同比特率下的输出电压作为时间的函数。因此,本文演示了第一个设计用于长寿命金星着陆器的基于sic的通信电路。
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First Iteration Communications Circuit for a Long-Lived In-situ Solar System Explorer (LLISSE)
The first iteration communication system circuitry for the Venus Long-Lived In-situ Solar System Explorer (LLISSE) lander was developed using NASA Glenn Research Center SiC JFET technology. The atmosphere of Venus is a harsh environment that experiences temperatures upward of 460 °C, pressures of 1344 psi, and a dense, corrosive atmosphere composed of CO2, N2, SO2, HF, HCl, CO, OCS, H2S, and H2O making Venus a challenging environment for electronics. Previous missions to Venus have lasted for less than two hours, but LLISSE is being planned and developed to survive 60 Earth days. The communications circuit was designed in Keysight Advance Design Systems (ADS), using three stages of differential amplifiers with the bias circuit designed to be turned on and off for On-Off Keying (OOK) modulation. Buffer amplifiers are integrated into the circuit to facilitate testing. Based on JFET SiC technology developed at NASA Glenn Research Center, it's designed to operate at 5 MHz at room temperature, and 2 MHz at 460 °C. OOK gives the advantage of low power consumption and is ideal for the low frequency transmission. The SiC JFET has been shown to survive 60 days in a simulated Venusian environment. The circuits are tested in the laboratory on a high temperature probe station. The die is mounted and wirebonded on an alumina carrier for probing. Two output ports provide positive and negatively swinging signals to supply a balanced signal to the antenna; the input ports are for bias and a control signal that will come from a digital output of the sensors. The oscillation frequency, output power, phase noise, and data rate are measured as a function of temperature. The output power and phase noise are shown as a function of frequency. The output voltage is measured as a function of time at room temperature and Venus temperature for different bit rates. As a result, this paper demonstrates the first SiC-based communication circuit designed to operate on a long-lived Venus lander.
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