SM: Service module DS: Descent stage (lander) AS: Ascent stage AD: Adapter DA: Docking adapter RV: Reentry vehicle
-
Diesen Thread anzeigen
-
At launch, the stack has the AS on top of the DS on top of the AD on top of the SM, wit the DA on top of the RV sitting on the SM inside the AD.
3 Antworten 2 Retweets 39 Gefällt mirDiesen Thread anzeigen -
The phases: 1) Possibly, phasing Earth orbits prior to translunar injection (awaiting clarification). 2) Translunar injection and coast 3) Lunar orbit insertion, maybe to elliptical orbit. 4) Lunar orbit manuevers to low circular lunar orbit. (continued)..
1 Antwort 1 Retweet 33 Gefällt mirDiesen Thread anzeigen -
5) DS+AS separate from SM+AD, in lunar orbit. 6) AD is ejected from SM, revealing DA+RV attached to SM. AD remains in lunar orbit. 7) DS+AS land on Moon and obtain sample, placed in AS 8) AS takes off, leaving DS on moon. (continued)
2 Antworten 0 Retweets 31 Gefällt mirDiesen Thread anzeigen -
9) AS enters lunar orbit and makes rendezvous burns 10) AS docks with the DA on the SM 11) DA mechanism transfers sample from AS to RV 12) AS+DA ejected from the SM+RV. AS+DA remain in lunar orbit. (continued)
1 Antwort 1 Retweet 35 Gefällt mirDiesen Thread anzeigen -
13) SM+RV move to elliptical lunar orbit. 14) SM makes trans-earth insertion burn 15) SM+RV trans-earth coast. 16) RV separates from SM (continued)
1 Antwort 0 Retweets 31 Gefällt mirDiesen Thread anzeigen -
17) SM *either* burns up on Earth atmo entry *or* performs avoidance burn to begin new extended mission. 18) RV hypervelocity atmo entry, jettison aeroshell, deploy parachute, lands in China (Inner Mongolia province). (continued)
3 Antworten 0 Retweets 28 Gefällt mirDiesen Thread anzeigen -
19) The AS+DA, and separately the AD, remain in low lunar orbit until mascons perturb them to impact the lunar surface (probably of order 1 year?)
1 Antwort 1 Retweet 36 Gefällt mirDiesen Thread anzeigen -
Next challenge: what is the breakdown of the wet and dry masses of each of these components, totalling 8200 kg at launch? I solicit estimates.
7 Antworten 1 Retweet 40 Gefällt mirDiesen Thread anzeigen -
Antwort an @planet4589
I have found a Chinese paper that gives the orbiter (w/ return capsule probably since it's about the docking mechanism) total mass as 3066 kg & the ascent stage at 509 kg. The paper is from December 2013 though so figures may vary since then.
2 Antworten 1 Retweet 4 Gefällt mir
Source: Xu Z G, Yang M Y, He Y, et al. Research on pose optimal sliding mode control method for six DOF air-bearing spacecraft simulator (in Chinese). Chin Sci Bull (Chin Ver), 2013, 58(Suppl. II): 121–127, doi: 10.1360/972013-937
Das Laden scheint etwas zu dauern.
Twitter ist möglicherweise überlastet oder hat einen vorübergehenden Schluckauf. Probiere es erneut oder besuche Twitter Status für weitere Informationen.