A few LADEE Videos

I’m busy working the LADEE mission these days, and I’ve got some stuff coming on it (as soon as I get it cleared by NASA). In the mean time, 2 videos already up on LADEE:

An overview:

And a bit more showing some of the propulsion system:

And while the last video mentions that LADEE will use “a low altitude, retrograde, circular orbit. The most complex Lunar flight path attempted since the Apollo missions”, they don’t even show the cool part (my part), which is the cislunar trajectory. It’s coming….

Russians to Decide Fate of Express-AM4

Astrogator Mike has worked a lot recently on a re-purposing plan for the Express-AM4 spacecraft, and is quoted extensively in this article.

Don’t splash the bird!

Russians to decide on Polar Broadband Plan

This could be a great mission for science, and involved some decent Earth-orbiting astrogation. Stay tuned for more details of this orbit once we hear the fate of the bird. Don’t miss the associated video here:

This video shows the orbit-raising plan.

Earth Asteroid Imacts: The Earth Risk Corridor

The following is from Dan Adamo, guest astrogator and a former Flight Dynamics Officer at JSC. Dan runs a mail list called the ATIG (Astrodynamics Technical Interchange Group). Last year he graciously allowed me(Mike) to be a part of the group, and since then I get interesting articles from him every month or so. This month, Dan sent the following, which I thought was a great topic for the guild.


Dan Adamo

Earth Risk Corridor Computations for 2011 AG5 on 5 February 2040

Introduction

The near-Earth object (NEO) designated 2011 AG5 is currently associated with a relatively high linearized Earth impact probability of 0.001557 (odds of 1-in-642.3) during its predicted 5 February 2040 close approach to Earth. This probability appears in Table 1 (reference the P_i/p column), together with data pertaining to other near-term 2011 AG5 planetary approaches closer than 0.1 AU (15 million km). These predictions are obtained from JPL’s Horizons on-line solar system data and ephemeris computation service* using the current JPL#45 orbit solution for 2011 AG5. Note that coordinate time (CT) is a uniform time scale void of leap seconds and used as the fundamental ephemeris argument by Horizons. To a precision of ±0.002 s, CT is related to atomic time (TAI) by CT = TAI + 32.184 s.

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