VHSS

Venus Horizon
Satellite Systems

Building Equipment so Tough, that It Survives Venus

Landing Phase

High Altitude

The orbital descent will take place over several days as the probe builds the momentum necessary to slowly decrease orbital altitude. Aerobraking will be employed as much as possible as the Venusian atmosphere thickens.

Medium Altitude

At approximately 250km of altitude, the upper part of the atmosphere, a drag parachute will deploy. The probe will slow to below supersonic speeds. At approximately 65km of altitude, the parachute will release and the probe will commence free fall to the surface.

Ground Approach

The Venusian atmosphere quickly thickens from 65km to the surface. The expected descent rate in the lower atmosphere is 10m/s. The probe is structurally hardened such that approaches near this velocity will ensure survival.

The graphic below illustrates the key points of entry into the Venus atmosphere. Unlike the Curiosity Mars rover pictured here, following parachute separation, our lander will coast through the very dense atmosphere for the final 65km and touch down without the need for an elaborate landing system. Touch down is on 07SEP2018, 50 days before inferior conjuction. There will then be 5 days to complete drilling for proper seismograph placement and charging the batteries at ambient temperature. Following that, line-of-sight communications will be available with Earth and the primary science mission will begin.

Descent Phase
Image courtesy of NASA http://www.nasa.gov/images/content/667372main_MSL%20EDL%20rev-2900.jpg

Communication Impact of Landing Site

Based on the orbital speeds of Earth and Venus, selecting a site on the equator will give an elevation angle for line-of-sight communications that should never be more than a maximum of 67 degrees below zenith. This corresponds to 180km of Venusian atmosphere that signals will have to pass through to successfully communicate.