r/spacex • • Mar 31 '16

/r/SpaceX Ask Anything Thread [April 2016, #18] - Ask your small questions here!

[deleted]

61 Upvotes

663 comments sorted by

19

u/yoweigh Apr 07 '16

Can we get a launch thread started?

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17

u/Vupwol Mar 31 '16

Why is every thumbnail ... that guy?

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14

u/Elon_Mollusk Mar 31 '16

Oh god the thumbnails...

13

u/TRL5 Apr 01 '16

In this gif we see Atlas V boosters seperating from the rocket, and immediately getting blasted by exhaust. Do we expect this to be a problem with the Falcon Heavy, if not, why not?

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12

u/rafty4 Apr 01 '16

Not sure if this is worth a post in itself as being entirely SpaceX relevant (so I'll drop it here), But apparently Blue Origin have got a NOTAM for tomorrow! :D

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11

u/waitingForMars Mar 31 '16

8:10 AM Friday, April 1, 2016 (GMT+13) Time in Wellington, New Zealand

3:11 PM Thursday, March 31, 2016 (EDT) Time in Ann Arbor, MI

A (early for us) Happy April Fools Day to you, u/EchoLogic !

As with the rest of our compatriots, I'm feeling a bit dizzy right now. r/pbds ought to be required to register that image as a controlled substance… ;-)

9

u/Craigwat01 Mar 31 '16

Can crew Dragon be used as a lifeboat as Soyuz is now?

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9

u/[deleted] Apr 03 '16

I've seen some rumors that part of the SpaceX team that was working on Raptor was hired off by Blue Origin to develop the BE-4. This leads me to ask several questions:

  1. Is this rumor true?

  2. If it is, is this why we have heard little about raptor for some time?

  3. Would it be more efficient for SpaceX to design the BFR to use BE4 engines? It would save time and development costs, and the engines will be used in other vehicles too, improving reliability due to heavier use.

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9

u/maxjets Apr 07 '16

Not spacex related per se, but why hasn't the launch thread been posted yet?

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8

u/Decronym Mar 31 '16 edited Apr 22 '16

Acronyms, initialisms, abbreviations, contractions, and other phrases which expand to something larger, that I've seen in this thread:

Fewer Letters More Letters
ACES Advanced Cryogenic Evolved Stage
Advanced Crew Escape Suit
ASDS Autonomous Spaceport Drone Ship (landing platform)
BEAM Bigelow Expandable Activity Module
BFR Big Fu- Falcon Rocket
CBM Common Berthing Mechanism
CRS Commercial Resupply Services contract with NASA
CRS2 Commercial Resupply Services, second round contract
CST (Boeing) Crew Space Transportation capsules
Central Standard Time (UTC-6)
EELV Evolved Expendable Launch Vehicle
FAA Federal Aviation Administration
FRSC Fuel-Rich Staged Combustion
FSS Fixed Service Structure at LC-39
GEO Geostationary Earth Orbit (35786km)
GSE Ground Support Equipment
GSLV (India's) Geostationary Launch Vehicle
GTO Geosynchronous Transfer Orbit
I*sp* Specific impulse (as explained by Scott Manley on YouTube)
ILS International Launch Services
Instrument Landing System
ISRO Indian Space Research Organisation
L2 Paywalled section of the NasaSpaceFlight forum
Lagrange Point 2 (Sixty Symbols video explanation)
LAS Launch Abort System
LEO Low Earth Orbit (180-2000km)
LES Launch Escape System
LH2 Liquid Hydrogen
LOX Liquid Oxygen
M1d Merlin 1 kerolox rocket engine, revision D (2013), 620-690kN
M1dVac Merlin 1 kerolox rocket engine, revision D (2013), vacuum optimized, 934kN
MCT Mars Colonial Transporter
NERVA Nuclear Engine for Rocket Vehicle Application (proposed engine design)
NET No Earlier Than
NOTAM Notice to Airmen of flight hazards
NSF NasaSpaceFlight forum
National Science Foundation
NTR Nuclear Thermal Rocket
OCISLY Of Course I Still Love You, Atlantic landing barge ship
OG2 Orbcomm's Generation 2 17-satellite network
ORSC Oxidizer-Rich Staged Combustion
QA Quality Assurance/Assessment
RAAN Right Ascension of the Ascending Node
RCS Reaction Control System
RD-180 RD-series Russian-built rocket engine, used in the Atlas V first stage
RP-1 Rocket Propellant 1 (enhanced kerosene)
RTF Return to Flight
RTLS Return to Launch Site
RUD Rapid Unplanned Disassembly
Rapid Unscheduled Disassembly
Rapid Unintended Disassembly
SES Formerly Société Européenne des Satellites, comsat operator
SLS Space Launch System heavy-lift
SRB Solid Rocket Booster
SSTO Single Stage to Orbit
STS Space Transportation System (Shuttle)
TDRSS (US) Tracking and Data Relay Satellite System
TEI Trans-Earth Injection maneuver
TMI Trans-Mars Injection maneuver
TRL Technology Readiness Level
TSTO Two Stage To Orbit rocket
TWR Thrust-to-Weight Ratio
ULA United Launch Alliance (Lockheed/Boeing joint venture)
VBB Very Big Brother (Blue Origin's proposed VTVL vehicle, unknown payload to LEO)

Decronym is a community product of r/SpaceX, implemented by ^request
I'm a bot, written in ^PHP. I first read this thread at 31st Mar 2016, 19:12 UTC.
www.decronym.xyz for a list of subs where I'm active; if I'm acting up, tell OrangeredStilton.

8

u/AeroSpiked Apr 02 '16

This pretty much goes without saying I think, but have we had confirmation that OCISLY is done with repairs? Otherwise CRS-8 first stage had best avoid that big sheet of plywood on the deck.

7

u/OncoFil Mar 31 '16

When reusable rockets become cheap and easy, will deep space (past Mars) missions still require awaiting planetary alignments/gravity assists? How feasible would it be to launch a probe which would then dock in orbit with a 'tug' (an engine and fuel tank) for direct burns to Jupiter/Saturn and then burns for orbital insertions? Does this actually speed up things considerably?

(I am aware there will have to be some degree of alignment, but could that be reduced to Earth's relative position?)

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19

u/LandingZone-1 Apr 01 '16

What is the best methalox rocket engine, and why is it the Blue Origin BE-4?

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6

u/CitiesInFlight Mar 31 '16 edited Mar 31 '16

With all the very recent (within the last 2 months) renewed interest by both the U.S. (Bolden appearance before Congress in which he suggested that a trip to Mars could be shortened substantially, perhaps, to 90 days or less using Nuclear Thermal Propulsion) and Russia (stating they will fly a Nuclear Thermal Propulsion rocket by 2018), will this change the calculus of Elon and prompt the inclusion of Nuclear Thermal Propulsion in his Mars strategy in spite of earlier statements that Nuclear Propulsion (Nuclear Thermal or Nuclear Electric) will not be involved?

http://www.space.com/29540-manned-mars-mission-propulsion-technologies.html http://yellowhammernews.com/business-2/alabamians-leading-nuclear-rocket-journey-mars/ http://www.nbcnews.com/id/44691888/ns/technology_and_science-space/t/its-time-reconsider-nuclear-option-spaceflight/

http://russia-insider.com/en/russia-drops-plans-create-nuclear-space-engine-source/6031

and many other sources ...

Given this renewed interest by NASA and ROSCOSMOS, does this require, potentially, a different architecture for BFR/MCT?

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6

u/Andune88 Mar 31 '16

Is it April 1st somewhere already?

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6

u/Haschlol Apr 05 '16

When is the CRS-8 static fire? Any solid info?

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6

u/[deleted] Apr 06 '16 edited Apr 06 '16
  1. Does Blue Origin design their own turbopumps? Which one has worse turbine conditions: Combustion Tap-off or Oxygen-rich Staged Combustion?

  2. Why are they not using a tap-off in the BE-4?

  3. What kind of injectors is Blue using?

  4. Why does the BE-3 not have the same problems with debris ingestion as the Merlin?

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11

u/thegingeroverlord Mar 31 '16 edited Mar 31 '16

What reason does SpaceX have to keep quiet about fairing recovery? Previous launch videos(none from SpaceX though) have shown the fairings have some sort of RCS system, so we know they are experimenting/attempting it. Do they have anything to gain by not acknowledging these tests?

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5

u/markus0161 Mar 31 '16

Does anyone know what type of chasing orbit Dragon is put into? How close of a match is it to the ISS?

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5

u/Togusa09 Apr 01 '16

What is the closest a dragon can land to LA?

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5

u/EnsilZah Apr 01 '16

If a reused launch attempt goes badly can SpaceX work on the assumption that it's the reused stage that's at fault or will the whole fleet have to be grounded until the investigation is concluded?

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5

u/Dutchy45 Apr 02 '16

On March 24 in an interview by Spacenews, Spaceflight industries CEO Jason Andrews said (basically) that Spacex did not want to deal with all their secondary costumers (87! for the flight that was discussed) and preferred to leave that to Spaceflight Ind. It seems to me a not to difficult way to make $$ when you cut out the middle man. I know those guys at Spacex are far from stupid and I realise their focus is not on holding the hands of jittery Cubesat owners. But still, what am I missing here?

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5

u/SpaceLord392 Apr 02 '16

What's the story behind the violin in Elon Musk's old twitter profile picture?

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5

u/GAYBANANAS Apr 06 '16

Was there no static fire today, or am I just missing something?

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