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HP Prime G1: None HP Prime G1 (NW280AA, G8X92AA) 400 MHz Samsung S3C2416XH-40 (ARM926EJ core, ARMv5 architecture) 32 MB RAM, 256 MB flash 320×240 pixel 16-bit color multi-touch TFT LCD with backlight: Algebraic, Entry RPN: Fixed PPL: Xcas/Giac-based Unicode: No USB (USB-OTG only with G8X92AA model)
ISO 18265: "Metallic materials — Conversion of hardness values" (2013) ASTM E140-12B(2019)e1: "Standard Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness" (2019)
It is turbocharged and intercooled with a power output of 225 PS (165 kW; 222 hp) at 5700 rpm and 310 N⋅m (229 lb⋅ft) of torque at 2700–5100 rpm. It is equipped with Bosch Motronic 4.4 engine management for model years 1997 and 1998. It is equipped with Bosch ME7 for model years 1999 and 2000.
HP 40g (F1907A) was released in 2000 in parallel with the HP 39g. The HP 40g's operating system is identical to the HP 39g. Differences detected in hardware during start-up trigger the differences in software functionality. The hardware is identical to the HP 49G/39G series (complete with rubber keyboard).
The compression ratio in these engines was 17.2:1. The 1998–2000 ISB was rated at 215 hp (160 kW; 218 PS) and 420 lb⋅ft (569 N⋅m) when equipped with the 47RE automatic transmission. The 1998–2000 ISB was rated at 235 hp (175 kW; 238 PS) and 460 lb⋅ft (624 N⋅m) when equipped with a manual transmission.
The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel and stabilized aerodynamically. The original version, VS-40, uses the S-40TM (4,200 kg) first stage engine and the S-44M (810 kg) second stage engine. [2] [3] [4] This configuration corresponds to the upper stages of the VLS-1 rocket. [5]
The 22.5 cm Minenwerfer M 15 was a heavy mortar used by Austria-Hungary in World War I. [1] It was developed by Böhler as an alternative to the German Ehrhardt 25 cm schwere Minenwerfer which Böhler was having problems building under license. It was a muzzle-loading, smooth-bore mortar that had no recoil system whatsoever.
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