小型超音速無人飛行機を用いた飛行実験の成立性解 析 : 研究成果報告

小型超音速無人飛行機を用いた飛行実験の成立性解 析 : 研究成果報告

著者 木村  博幸, 溝端  一秀, 棚次  亘弘

雑誌名 室蘭工業大学航空宇宙機システム研究センター年次

報告書

巻 2005

ページ 66‑72

発行年 2006‑08

URL http://hdl.handle.net/10258/00008655

小型超音速無人飛行機を用いた飛行実験の成立性解 析 : 研究成果報告

著者 木村  博幸, 溝端  一秀, 棚次  亘弘

雑誌名 室蘭工業大学航空宇宙機システム研究センター年次

報告書

巻 2005

ページ 66‑72

発行年 2006‑08

URL http://hdl.handle.net/10258/00008655

66

ዊဳ⿥㖸ㅦήੱ㘧ⴕᯏ䉕↪䈇䈢㘧ⴕታ㛎䈱ᚑ┙ᕈ⸃ᨆ㩷 㵨㩷 ⎇ⓥᚑᨐႎ๔㩷

㩷 䂾ᧁ᧛㩷 ඳᐘ䋨↢↥ᖱႎ䉲䉴䊁䊛Ꮏቇኾ᡹㩷 ⥶ⓨቝቮᯏ䉲䉴䊁䊛⎇ⓥቶ䋩㩷

Ḵ┵㩷 ৻⑲䋨ᯏ᪾䉲䉴䊁䊛Ꮏቇ⑼㩷 ഥᢎ᝼䋩㩷

᫜ᰴ㩷 ਗ਼ᒄ䋨⥶ⓨቝቮᯏ䉲䉴䊁䊛⎇ⓥ䉶䊮䉺䊷㐳䋬ᢎ⢒⎇ⓥ╬ᡰេᯏ᭴㩷 ᢎ᝼䋩㩷 㩷 㩷

㪈㪅 䈲䈛䉄䈮㩷

ᧄ⎇ⓥߢߪ㧘⥶ⓨቝቮᯏࠪࠬ࠹ࡓ⎇ⓥ࠮ࡦ࠲࡯߇ផߒㅴ߼ߡ޿ࠆዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩ⎇ⓥ

㐿⊒ࡊࡠࠫࠚࠢ࠻[1]ߩ৻Ⅳߣߒߡ㧘

2005

ᐕᐲߦឭ᩺ߐࠇߚ

2

ߟߩ࠲ࠗࡊߩߘߩ╙

1

ᰴᯏ૕ᒻ⁁᩺

ߩ߁ߜ㧘࿕ቯᓟㅌⷺ⠢ᑼߩᯏ૕ߦ㑐ߔࠆ㘧ⴕ⚻〝⸃ᨆࠍታᣉߒ㧘หᯏࠍ↪޿ߚ㘧ⴕታ㛎ߩᚑ┙ᕈ ߩᬌ⸛ࠍⴕߞߚ㧚

㪉㪅 ዊဳ䉺䊷䊗䉳䉢䉾䊃䉣䊮䉳䊮䈱⻉ర䈫ᕈ⢻㩷

਄ㅀߩዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߦ៞タߐࠇࠆዊဳ࠲࡯ࡏࠫࠚ࠶࠻ࠛࡦࠫࡦߩᄖᓘߪ

220 mm㧘ߘߩ

ࠗࡦࡍ࡜࡯ߩ⋥ᓘߪ

170 mm

ߢ޽ࠆ㧚ߎߩࠛࡦࠫࡦߩ⸳⸘࿶❗Ყߪ

3.8㧘㊀㊂ផ▚୯ߪ45.3 kg

ߢ

޽ࠆ㧔⴫

1㧕

㧚1 ᰴరߩࠨࠗࠢ࡞⸃ᨆߦၮߠ޿ߡ੍஻⊛ߦផ▚ߐࠇߚߘߩផജᕈ⢻ࡑ࠶ࡊ㧘Ყផജ ᕈ⢻ࡑ࠶ࡊ㧘ๆ޿ㄟߺⓨ᳇ᵹ㊂ࡑ࠶ࡊࠍߘࠇߙࠇ࿑

1

ߩ(a), (b), (c)ߦ␜ߔ㧚࿾਄㕒ᱛ⁁ᘒߦ߅ߌࠆ

⴫

1 ዊဳ࠲࡯ࡏࠫࠚ࠶࠻ࠛࡦࠫࡦߩ઀᭽㧚

䉣䊮䉳䊮䈱ᄖᓘ㩷 㪇㪅㪉㪉㪇㩷㫄㩷

䉟䊮䊁䊷䉪䈱ᵹ〝ᓘ㩷 㪇㪅㪇㪇㪇㩷㵨㩷㪇㪅㪈㪌㪇㩷㫄㩷

࿶❗ᯏ౉ญ䈱ᵹ〝ᓘ㩷 㪇㪅㪇㪎㪇㩷㵨㩷㪇㪅㪈㪎㪇㩷㫄㩷

䉺䊷䊎䊮౉ญ䈱ᵹ〝ᓘ㩷 㪇㪅㪈㪉㪈㪌㩷㵨㩷㪇㪅㪈㪍㪇㩷㫄㩷

䊉䉵䊦಴ญ䈱ᵹ〝ᓘ㩷 㪇㪅㪇㪇㪇㩷㵨㩷㪇㪅㪈㪋㪇㪌㩷㫄㩷

࿶❗ᯏല₸㩷 㪇㪅㪏㪇㩷

䉺䊷䊎䊮ല₸㩷 㪇㪅㪏㪎㩷

࿶❗Ყ㩷 㪊㪅㪏㪇㪍㩷

ⓨ᳇ᵹ㊂䋨㪸㫋㩷㪪㪣㪪䋩㩷 㪊㪅㪌㪏㪏㩷㫂㪾㪆㫊㩷

㊀㊂㩷 㪋㪌㪅㪊㩷㫂㪾㩷

࿑

1 ዊဳ࠲࡯ࡏࠫࠚ࠶࠻ࠛࡦࠫࡦߩ૞േᕈ⢻㧚

㪈㪇

㪏

㪍

㪋

㪉

㪇

Altitude, km

㪉㪅㪇 㪈㪅㪌 㪈㪅㪇 㪇㪅㪌 㪇㪅㪇

Mach number 2,051 sec at SLS "Mu-170" - Isp - No A.B.

10 kPa

50 kPa 100 kPa

(b)

Ყផജᕈ⢻ࡑ࠶ࡊ㧚

㪈㪇

㪏

㪍

㪋

㪉

㪇

Altitude, km

㪉㪅㪇 㪈㪅㪌 㪈㪅㪇 㪇㪅㪌 㪇㪅㪇

Mach number "Mu-170" - Thrust - No A.B.

1.413 kN at SLS 10 kPa

50 kPa 100 kPa

(a)

ផജᕈ⢻ࡑ࠶ࡊ㧚

㪈㪇

㪏

㪍

㪋

㪉

㪇

Altitude, km

㪉㪅㪇 㪈㪅㪌 㪈㪅㪇 㪇㪅㪌 㪇㪅㪇

Mach number "Mu-170" - Mass flow rate of air - No A.B.

10 kPa

50 kPa 100 kPa

3.588 kg/s at SLS

(c)

ⓨ᳇ᵹ㊂ࡑ࠶ࡊ㧚

0XWXUERMHWHQJLQH :LWKRXWDIWHUEXUQHU 7KUXVWDW6/6NJI ,VSDW6/6VHF :LWKDIWHUEXUQHU)$

7KUXVWDW6/6NJI ,VSDW6/6VHF 0XWXUERMHWHQJLQH

&RPSUHVVRU2QHGLDJRQDO

&RPSUHVVLRQ5DWLR

&RPSUHVVRU(IILFLHQF\

7XUELQH(IILFLHQF\

0XWXUERMHWHQJLQH 2XWHUGLDPHWHUPP )DQGLDPHWHUPP (VWLPDWHGZHLJKWNJ

$LUIORZUDWHDW6/6NJV

หࠛࡦࠫࡦߩផജߪ

140 kgf㧘Ყផജߪ2,051 sec

ߢ޽ࠆ㧚߹ߚ㧘ΆⓨᲧ

0.03

ߢࠕࡈ࠲࡯ࡃ࡯࠽࡯

ࠍ૶↪ߒߚ႐วߩ࿾਄㕒ᱛ⁁ᘒߦ߅ߌࠆផജߪ

190 kgf㧘Ყផജߪ1,048 sec

ߢ޽ࠆ[2]㧚

㪊㪅 ዊဳ⿥㖸ㅦήੱ㘧ⴕᯏ䈱ᯏ૕ᒻ⁁䈫ⓨജ․ᕈ㩷

⸃ᨆኻ⽎ߣߔࠆዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩᯏ૕ᒻ⁁㧔࿕ቯᓟㅌⷺ⠢ᑼ㧕ࠍ࿑

2

ߦ㧘ߘߩ⻉రߣ㊀

㊂ផ▚୯ࠍ⴫

2

ߦ␜ߔ㧚ߎߩᯏ૕ߩో㐳ߪ

3 m㧘⢵૕ᓘߪ25 cm㧘⠢᏷ߪ1.33 m

ߢ޽ࠆ㧚⛔⸘⊛

ផ▚ᑼ[3]ߦၮߠ޿ߡᓧࠄࠇߚ㔌㒽㊀㊂ߩផ▚୯ߪ

271.4 kg

ߣߥߞߚ㧚JAXA ቝቮ⑼ቇ⎇ⓥᧄㇱߩ 㜞ㅦ᳇ᵹ✚วታ㛎⸳஻ࠍ೑↪ߒߡᓧࠄࠇߚหᯏߩᭂᦛ✢ࠍ࿑

3

ߦ␜ߔ㧚ห࿑ߩⓨജଥᢙߪ㧘ଏ⹜

૕ᮨဳߩࠛࡦࠫࡦᵹ〝߇㐽Ⴇߐࠇߚ⁁ᘒߢᓧࠄࠇߚ߽ߩߢ޽ࠆ[4]㧚

㪋㪅 ⸃ᨆᚻᴺ㩷

ᧄ⸃ᨆߢߪ㧘࿑

5

ߦ␜ߔࠃ߁ߥ࿾⃿ࠍਛᔃߣߔࠆ

3

⥄↱ᐲᘠᕈᭂᐳᮡ♽ࠍᗐቯߒ㧘ਅ⸥ߦ␜ߔ

⾰ὐ㧔㘧ⴕ૕㧕ߩㆇേᣇ⒟ᑼߦၮߠ޿ߡ㘧ⴕ⚻〝⸃ᨆࠍⴕߞߚ㧚ਅᑼߦ߅޿ߡ㧘r ߪ࿾ᔃ㜞ᐲ㧘

T

ߪ⚻ᐲ㧘

M

ߪ✲ᐲ㧘

m

ߪᯏ૕ߩ⾰㊂㧘F

_r/m, F_T/m, F_M/m

ߪߘࠇߙࠇ㜞ᐲᣇะ㧘⚻ᐲᣇะ㧘✲ᐲᣇะߩ ടㅦᐲ㧘

Z

ߪ࿾⃿ߩ⥄ォㅦᐲߢ޽ࠆ㧚ᯏ૕ߦߪ឴ജ㧘᛫ജ㧘ផജ߅ࠃ߮㊀ജ߇૞↪ߔࠆ߽ߩߣߒ㧘

࿾⃿ߩ⥄ォߦߟ޿ߡ߽⠨ᘦߒߚ㧚ਅ⸥ߩㅪ┙ᓸಽᣇ⒟ᑼߩ⸃ᴺߣߒߡߪ㧘ೞߺ᏷⥄േ⺞ᢛဳߩ

6

Ბ

5

ᰴ

Runge-Kutta-Fehlberg

ᴺ[5]ࠍ↪޿ߚ㧚

⴫

2

ዊဳ⿥㖸ㅦήੱ㘧ⴕᯏ㧔╙

1

ᰴ⸳⸘᩺㧘࿕ቯᓟㅌ

ⷺ⠢ᑼ㧕ߩਥߥ⻉రߣᯏ૕㊀㊂ߩផ▚୯

ᯏ૕䈱⻉ర㩷 㩷

ో㐳㪃㩷㫄㩷 㪊㪅㪇㩷

⢵૕ᓘ㪃㩷㫄㩷 㪇㪅㪉㪌㩷

⠢᏷㪃㩷㫄㩷 㪈㪅㪊㪊㩷

㜞䈘䋨㔌⌕㒽ⵝ⟎䉕㒰䈒䋩㩷 㪃㩷㫄㩷 㪇㪅㪌㪏㪊㩷

ⓨജᐔဋ⠢ᒏ㪃㩷㫄㩷 㪇㪅㪐㪇㪐㩷

ⓨജਛᔃ૏⟎䋨⢵૕వ┵ၮḰ䋩㪃㩷㩼㩷 㪍㪍㪅㪊㩷

⠢㕙Ⓧ㪃㩷㫄

^㪉

㩷 㪇㪅㪐㪎㪉㩷

ਥ⠢೨✼ᓟㅌⷺ㪃㩷㪻㪼㪾㪅㩷 㪋㪌㪃㩷㪎㪇㩷

ਥ⠢䉝䉴䊕䉪䊃Ყ㩷 㪈㪅㪋㪍㩷

ᯏ૕㊀㊂䈱ផ▚୯㩷 㩷

Άᢱ㊀㊂㪃㩷㫂㪾㩷 㪋㪌㪅㪇㩷

ੇ῎㊀㊂㪃㩷㫂㪾㩷 㪉㪉㪍㪅㪋㩷

㔌㒽㊀㊂㪃㩷㫂㪾㩷 㪉㪎㪈㪅㪋㩷

࿑

2 ዊဳ⿥㖸ㅦήੱᯏ㧔╙1

ᰴ⸳⸘᩺㧘࿕ቯᓟㅌ

ⷺ⠢ᑼ㧕ߩᯏ૕ᒻ⁁㧚

㪈㪅㪇 㪇㪅㪏 㪇㪅㪍 㪇㪅㪋 㪇㪅㪉 㪇㪅㪇 㪄㪇㪅㪉 㪄㪇㪅㪋

㪣㫀㪽㫋㩷㪺㫆㪼㪽㪽㪅㪃㩷㪚㪣

㪇㪅㪈㪋 㪇㪅㪈㪉 㪇㪅㪈㪇 㪇㪅㪇㪏 㪇㪅㪇㪍 㪇㪅㪇㪋 㪇㪅㪇㪉 㪇㪅㪇㪇

㪛㫉㪸㪾㩷㪺㫆㪼㪽㪽㪅㪃㩷㪚㪛 㩷 㩷㪤㪇㪅㪊

㩷 㩷㪤㪇㪅㪎 㩷 㩷㪤㪇㪅㪐 㩷 㩷㪤㪈㪅㪈 㩷 㩷㪤㪈㪅㪉 㩷 㩷㪤㪈㪅㪊 㩷 㩷㪤㪈㪅㪌 㩷 㩷㪤㪈㪅㪎 㩷 㩷㪤㪈㪅㪐㩷 㪤㪄㫋㫐㫇㪼

㪇㩷㪘㫆㪘 㪉 㪄㪉

㪋 㪍 㩿㪥㫆㩷㪸㫀㫉㪄㪹㫉㪼㪸㫋㪿㫀㫅㪾㪀

㪤 ဳᯏ૕ᒻ⁁㩷

䊶ਥ⠢೨✼ᓟㅌⷺ 㪋㪌㩷㪻㪼㪾㪅䋨䉴䊃䊧䉟䉪ㇱ䋺㪎㪇㩷㪻㪼㪾㪅䋩㩷 䊶㪩㪼㩷㪔㩷㪈㪅㪉㩷㵨㩷㪊㪅㪈㬍㪈㪇

^㪎

㩷㪈㪆㫄㩷

䊶䉣䊮䉳䊮ౝㇱ䈱ⓨ᳇ๆ䈇ㄟ䉂ᮨᡆ䋺䈭䈚㩷

࿑

3

㘑ᵢ⹜㛎ߢᓧࠄࠇߚዊဳ⿥㖸ㅦήੱ㘧ⴕᯏ

㧔╙

1

ᰴ⸳⸘᩺㧘࿕ቯᓟㅌⷺ⠢ᑼ㧕ߩᭂᦛ✢㧚

68

⚻〝⸃ᨆߦ߅ߌࠆዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩ㘧ⴕࡊࡠࡈࠔࠗ࡞ߪਅ⸥ߩㅢࠅߢ޽ࠆ㧚หᯏߪ㧘Ṗ

⿛〝਄ߢ࿕૕ࡠࠤ࠶࠻ߦࠃࠆടㅦᡰេࠍᓧߡ㔌㒽ߒ㧘ߘߩᓟߪ៞タߐࠇߚ࠲࡯ࡏࠫࠚ࠶࠻ࠛࡦࠫ

ࡦߩផജߩߺߢടㅦ࡮਄᣹㘧ⴕߔࠆߎߣߦࠃߞߡ㧘⋡ᮡߣߔࠆ㘧ⴕࡑ࠶ࡂᢙ

1.4

߳ߩ೔㆐ࠍ⋡ᜰ ߔ㧚⋡ᮡ㘧ⴕࡑ࠶ࡂᢙߦ೔㆐ߒߚᓟߪ㧘ᷫㅦ࡮ᣓ࿁ߔࠆߎߣߦࠃߞߡ㧘኿႐߹ߢߩᏫㆶ㘧ⴕࠍ⹜

ߺࠆ㧚㘧ⴕታ㛎ߩ኿႐ߣߒߡߪർᶏ㆏ᄢ᮸↸ߩᄙ⋡⊛⥶ⓨ౏࿦ߩṖ⿛〝㧔࿑

6㧕ࠍᗐቯߔࠆ㧚

ߎߎߢ㧘਄ㅀߩⓨജଥᢙߪ㧘㘑ᵢ⹜㛎ߦ߅޿ߡଏ⹜૕ᮨဳߩࠛࡦࠫࡦᵹ〝߇㐽Ⴇߐࠇߚ⁁ᘒߢ ขᓧߐࠇߚ߽ߩߢ޽ࠆߎߣ߆ࠄ[4]㧘ᧄ⸃ᨆߦ߅޿ߡߪ㧘ታ㘧ⴕᤨߩ᛫ജଥᢙߩ୯߇ࠛࡦࠫࡦᵹ〝

㐽Ⴇᤨߩ

50 %߹ߢૐᷫߔࠆߣ޿߁઒ቯࠍ⸳ߌߚ㧚

㪌㪅 ⸃ᨆ⚿ᨐ㩷

㪌㪅㪈㪅㩷 ⸃ᨆ⚿ᨐ 㪈䋺㩷 ടㅦ㘧ⴕ䊚䉾䉲䊢䊮䋨䉝䊐䉺䊷䊋䊷䊅䊷䉕૶↪䈚䈢႐ว䋩㩷

⚻〝⸃ᨆߩ⚿ᨐ㧘ㆫ㖸ㅦၞ߆ࠄ⿥㖸ㅦၞߦ߆ߌߡࠕࡈ࠲࡯ࡃ࡯࠽࡯㧔ΆⓨᲧ

0.03㧕ࠍ૶↪ߒ㧘

㜞ᐲ

10 km

ߢㆫ㖸ㅦࠍㅢㆊߒߚ႐วߦ㧘⋡ᮡߣߔࠆ㘧ⴕࡑ࠶ࡂᢙ

1.4

ߦ೔㆐ߒᓧࠆߎߣ߇੍᷹ߐ

ࠇߚ㧔⴫

2㧘࿑6 (a)㧕㧚ߎߩߣ߈ߩ㘧ⴕ⚻〝ߩ㠽⍑࿑ߣ㧘㘧ⴕࡑ࠶ࡂᢙ㧘㘧ⴕേ࿶㧘ᯏ૕ߩᆫ൓ⷺ㧘

ᯏ૕ߦ૞↪ߔࠆⓨ᳇ജ╬ߩᤨ㑆⊛ផ⒖ࠍ࿑

6

ߦ߹ߣ߼ࠆ㧚Mach 1.4 ೔㆐ᤨߩ㘧ⴕᤨ㑆ߪ

600

⑽㧘 㘧ⴕ〒㔌ߪ

159 km㧘Άᢱᱷ㊂ߪ3.5 kg

ߢ㧘⿥㖸ㅦ㘧ⴕᤨߩㄫⷺߪ߅ࠃߘ

2 deg.ߢ޽ߞߚ[4]㧚

㪌㪅㪉㪅㩷 ⸃ᨆ⚿ᨐ 㪉䋺㩷 ടㅦ䊶Ꮻㆶ㘧ⴕ䊚䉾䉲䊢䊮䋨䉝䊐䉺䊷䊋䊷䊅䊷䉕૶↪䋩㩷

࿑

4

㘧ⴕ⚻〝⸃ᨆߢᗐቯߒߚ

3

⥄↱ᐲᘠᕈᭂᐳᮡ♽㧚

O =

࿾⃿ߩਛᔃ㧚

Z =

࿾⃿ߩ⥄ォㅦᐲ㧚

Z =

࿾⃿ߩ⥄ォゲ㧚

m =

ᯏ૕ߩ⾰㊂㧚

r =

࿾ᔃ㜞ᐲ㧚

Fr/m = r

ᣇะߩᯏ૕ߩടㅦᐲ㧚

T =

⚻ᐲ㧚

FT/m = T

ᣇะߩᯏ૕ߩടㅦᐲ㧚

M =

✲ᐲ㧚

FM/m = M

ᣇะߩᯏ૕ߩടㅦᐲ㧚

࿑

5 㘧ⴕታ㛎ߩ኿႐ߣߒߡᗐቯߒߚർᶏ㆏ᄢ᮸↸ᄙ

⋡⊛⥶ⓨ౏࿦ߩṖ⿛〝㧚

⚻ᐲ㧦

143.43 degE

✲ᐲ㧦42.48 degN

ᮡ㜞㧦15.24 m

. sin

cos 2

, sin

2 cos cos

2

,

cos^{2 2}

2

m F r

r r

m F r

r r

m F r r

r _r

M T

M M T M M

M M T M T M T

M M T

Z

t

T

T

₀

਄ㅀߩടㅦ㘧ⴕ᧦ઙߩਅߢ㧘Mach 1.4 ߦ೔㆐ߒߚ⋥ᓟߦ኿႐߳ߩᏫㆶࠍ⹜ߺߚ႐วߩ㠽⍑࿑ߣ

⸃ᨆ⚿ᨐࠍ࿑

7

ߦ␜ߔ㧚Mach 1.4 ೔㆐ᓟ㧘ࡃࡦࠢⷺ

45 deg.ߢฝᣓ࿁ࠍߒߡ኿႐߳ߩᏫㆶࠍ⋡ᜰߒ

ߚ߇㧘ᣓ࿁ᓟߔߋߦΆᢱ߇ዧ߈ߚߚ߼ߦ኿႐߳ߩᏫㆶߪ࿎㔍ߢ޽ࠆߣ޿߁⚿ᨐ߇ᓧࠄࠇߚ㧚ߎߩ ࠃ߁ߥᏫㆶ㘧ⴕࡒ࠶࡚ࠪࡦࠍ㆐ᚑߔࠆߚ߼ߦߪ㧘ടㅦ㘧ⴕᤨߩΆᢱᶖ⾌㊂ࠍシᷫߔࠆߚ߼ߦ㧘ᯏ

૕᛫ജࠍᄢ᏷ߦૐᷫߔࠆ㧔ടㅦ㘧ⴕᤨߩടㅦᕈ⢻ࠍ㜞߼ࠆ㧕ߥߤߩኻ╷߇ᔅⷐߣߥࠆ㧚

ᦝߦ㧘਄ㅀߩ㘧ⴕ᧦ઙߩਅߢ㧘ᯏ૕ߩ᭴ㅧ㊀㊂ߩ৻ㇱࠍ៞タΆᢱߩ㊀㊂ߦ⟎߈឵߃ࠆߎߣࠍᗐ ቯߒߡ⸃ᨆߒߚ⚿ᨐࠍ࿑

8

ߦ␜ߔ㧚ߘߩ⚿ᨐ㧘ᯏ૕ߩ᭴ㅧ㊀㊂ߩ߁ߜ

18 kg

ࠍ៞タΆᢱ㊀㊂ߦ⟎

߈឵߃ߚ႐วߦᏫㆶ㘧ⴕࡒ࠶࡚ࠪࡦࠍ㆐ᚑߒᓧࠆߎߣ߇੍᷹ߐࠇߚ㧚ߎߩ႐วߩᏫㆶᤨߩ㘧ⴕᤨ

㑆ߪ

1,506

⑽㧘㘧ⴕ〒㔌ߪ

364 km

ߢ޽ߞߚ[4]㧚

(e)

㘧ⴕ㜞ᐲߩផ⒖㧚

㪈㪉

㪈㪇

㪏 㪍

㪋

㪉

㪇

Altitude, km

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec K-04B-D25: 05WT CD50% H10 10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.4 㪉㪅㪇

㪈㪅㪌

㪈㪅㪇

㪇㪅㪌

㪇㪅㪇

Mach number

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec

㪏

㪍

㪋

㪉

㪇

Acceleration, G

Mach number Acceleration K-04B-D25: 05WT CD50% H10 10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.4

(c)

㘧ⴕࡑ࠶ࡂᢙߣ㘧ⴕടㅦᐲ ߩផ⒖㧚

㪏㪇

㪍㪇

㪋㪇

㪉㪇

㪇

Dynamic pressure, kPa

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec K-04B-D25: 05WT CD50% H10 10 km at transonic

Mach 1

with A.B., F/A = 0.030 Mach 1.2 S.B. peak

Mach 1.4

(d)

㘧ⴕേ࿶ߩផ⒖㧚

㪋

㪊

㪉

㪈

㪇

Thrust, kN

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec

㪋㪇㪇㪇

㪊㪇㪇㪇

㪉㪇㪇㪇

㪈㪇㪇㪇

㪇

Specific impulse, sec

K-04B-D25: 05WT CD50% H10 Thrust Isp 10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.4

(f)

ផജߣᲧផജߩផ⒖㧚

㪊㪇 㪉㪌 㪉㪇 㪈㪌 㪈㪇 㪌 㪇 㪄㪌 㪄㪈㪇

Angle of attack, deg.

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec

㪍㪇 㪌㪇 㪋㪇 㪊㪇 㪉㪇 㪈㪇 㪇 㪄㪈㪇 㪄㪉㪇

Flight path angle, Bank angle, deg.

Angle of attack Bank angle Flightpath angle K-04B-D25: 05WT CD50% H10 10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.4

(g)

ᯏ૕ߩᆫ൓ⷺߩផ⒖㧚

㪍

㪌

㪋 㪊

㪉

㪈

㪇

Forces, kN

㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec K-04B-D25: 05WT CD50% H10 Lift

Drag Weight Thrust 10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.4

(h)

ᯏ૕ߦ૞↪ߔࠆജߩផ⒖㧚

㪈㪉

㪈㪇

㪏

㪍

㪋

㪉

㪇

Altitude, km

㪉㪅㪇 㪈㪅㪌 㪈㪅㪇 㪇㪅㪌 㪇㪅㪇

Mach number K-04B-D25: 05WT CD50%

S.B. peak

D.P. 10 kPa

D.P. 50 kPa

D.P. 100 kPa

with A.B., F/A = 0.030 Mach 1

10 km, Mach 1.45

6 km, Mach 1.19 8 km, Mach 1.29

Mach 1.4

(a)

㜞ᐲ-ࡑ࠶ࡂᢙᐔ㕙਄ߦ߅ߌࠆ⸃ᨆ⚻〝㧚

(b)

⸃ᨆ⚻〝ߩ㠽⍑࿑㧚

࿑

6 ࿕ቯᓟㅌⷺ⠢ᑼዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߦ㑐ߔࠆ㘧ⴕ⚻〝⸃ᨆ⚿ᨐ㧔ടㅦ㘧ⴕࡒ࠶࡚ࠪࡦߩߺ㧕

㧧ࠕࡈ࠲࡯

ࡃ࡯࠽࡯㧔ΆⓨᲧ

0.03㧕ࠍ૶↪㧚

70

࿑

8

࿕ቯᓟㅌⷺ⠢ᑼዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߦ㑐ߔࠆ㘧ⴕ⚻〝⸃ᨆ⚿ᨐ㧔ടㅦ㘧ⴕࡒ࠶࡚ࠪࡦ㧗Ꮻㆶ㘧ⴕࡒ࠶

࡚ࠪࡦ㧕 㧧ࠕࡈ࠲࡯ࡃ࡯࠽࡯㧔ΆⓨᲧ

0.03㧕ࠍ૶↪㧧ᯏ૕᭴ㅧ㊀㊂ߩ߁ߜ㧘18 kg

ࠍ៞タΆᢱߦ⟎߈឵߃ߚ႐ว㧚

(a)

㘧ⴕ⚻〝ߩ㠽⍑࿑㧚

㪉㪅㪇

㪈㪅㪌

㪈㪅㪇

㪇㪅㪌

㪇㪅㪇

Mach number

㪈㪍㪇㪇 㪈㪋㪇㪇 㪈㪉㪇㪇 㪈㪇㪇㪇 㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec

㪏

㪍

㪋

㪉

㪇

Acceleration, G

Mach number Acceleration K-04B-D25: 05WT CD50%

10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.40

(b)

㘧ⴕࡑ࠶ࡂᢙߣ㘧ⴕടㅦᐲߩផ⒖㧚

㪊㪇 㪉㪌 㪉㪇 㪈㪌 㪈㪇 㪌 㪇 㪄㪌 㪄㪈㪇

Angle of attack, deg.

㪈㪍㪇㪇 㪈㪋㪇㪇 㪈㪉㪇㪇 㪈㪇㪇㪇 㪏㪇㪇 㪍㪇㪇 㪋㪇㪇 㪉㪇㪇 㪇

Time, sec

㪍㪇 㪌㪇 㪋㪇 㪊㪇 㪉㪇 㪈㪇 㪇 㪄㪈㪇 㪄㪉㪇

Flight path angle, Bank angle, deg.

Angle of attack Bank angle Flight path angle K-04B-D25: 05WT CD50%

10 km at transonic

Mach 1.2 S.B. peak

with A.B., F/A = 0.030 Mach 1

Mach 1.40

(c)

ᯏ૕ߩᆫ൓ⷺߩផ⒖㧚

࿑

7

࿕ቯᓟㅌⷺ⠢ᑼዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߦ㑐ߔࠆ㘧ⴕ⚻〝⸃ᨆ⚿ᨐ㧔ടㅦ㘧ⴕࡒ࠶࡚ࠪࡦ㧗Ꮻㆶ㘧ⴕࡒ࠶

࡚ࠪࡦ㧕 㧧ࠕࡈ࠲࡯ࡃ࡯࠽࡯㧔ΆⓨᲧ

0.03㧕ࠍ૶↪㧚

⴫

3

⸃ᨆ᧦ઙߣ⸃ᨆ⚿ᨐ㧚

᛫ജଥᢙ䈱⵬ᱜ₸

^㪁㪋

㪃㩷㩼㩷 㪌㪇㩷 㪌㪇㩷 㪌㪇㩷 㪌㪇㩷

䊚䉾䉲䊢䊮ᒻᘒ㩷 ടㅦ㘧ⴕ㩷 ടㅦ㘧ⴕ㩷 ടㅦ㘧ⴕ㩷 ടㅦ䊶Ꮻㆶ㘧ⴕ㩷

ㆫ㖸ㅦㅢㆊ㜞ᐲ㪃㩷㫂㫄㩷 㪍㪅㪇㩷 㪏㪅㪇㩷 㪈㪇㪅㪇㩷 㪈㪇㪅㪇㩷

䉝䊐䉺䊷䊋䊷䊅䊷䋨ΆⓨᲧ䋩㩷 㫆㫅㩷㩿㪇㪅㪇㪊㪀㩷 㫆㫅㩷㩿㪇㪅㪇㪊㪀㩷 㫆㫅㩷㩿㪇㪅㪇㪊㪀㩷 㫆㫅㩷㩿㪇㪅㪇㪊㪀㩷

ੇ῎㊀㊂㪃㩷㫂㪾㩷 㪉㪉㪍㪅㪋㩷 㪉㪉㪍㪅㪋㩷 㪉㪉㪍㪅㪋㩷 㪉㪇㪏㪅㪋㩷

៞タΆᢱ㊀㊂㪃㩷㫂㪾㩷 㪋㪌㪅㪇㩷 㪋㪌㪅㪇㩷 㪋㪌㪅㪇㩷 㪍㪊㪅㪇㩷

㔌㒽㊀㊂㪃㩷㫂㪾㩷 㪉㪎㪈㪅㪋㩷 㪉㪎㪈㪅㪋㩷 㪉㪎㪈㪅㪋㩷 㪉㪎㪈㪅㪋㩷

㘧ⴕᤨ㑆㪃㩷㫊㪼㪺㩷 㪊㪊㪊㩷 㪋㪎㪋㩷 㪍㪉㪋㩷㩿㪍㪇㪇㪀㩷 㪈㪌㪇㪍㩷

೔㆐㘧ⴕ䊙䉾䊊ᢙ㩷 㪈㪅㪈㪐㩷 㪈㪅㪉㪐㩷 㪈㪅㪋㪌㩷㩿㪈㪅㪋㪇㪀㩷 㪈㪅㪋㪇㩷

ᦨᄢ㘧ⴕേ࿶㪃㩷㫂㪧㪸㩷 㪋㪎㪅㪈㩷 㪋㪈㪅㪈㩷 㪊㪏㪅㪊㩷 㪊㪏㪅㪊㩷

㘧ⴕ〒㔌㪃㩷㫂㫄㩷 㪈㪇㪇㩷 㪈㪊㪋㩷 㪈㪍㪐㩷㩿㪈㪌㪐㪀㩷 㪊㪍㪋㩷

೔㆐㜞ᐲ㪃㩷㫂㫄㩷 㪍㪅㪇㩷 㪏㪅㪇㩷 㪈㪇㪅㪇㩷㩿㪈㪇㪅㪇㪀㩷 㪈㪇㪅㪇㩷

㪤㪸㪺㪿㩷㪈㪅㪋 ೔㆐ᤨ䈱Άᢱᱷ㊂㪃㩷㫂㪾㩷 㪄㩷 㪄㩷 㪊㪅㪌㩷 㪉㪈㪅㪌㩷

㔌㒽Ṗ⿛〒㔌㪃㩷㫂㫄㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷

㔌㒽ᤨ䈱ᔅⷐㄫⷺ㪃㩷㪻㪼㪾㪅㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷 㪇㪅㪈㪊㪍㩷

㪍㪅 䉁䈫䉄㩷

ᧄ⎇ⓥߢߪ㧘2005 ᐕᐲߦឭ᩺ߐࠇߚ࿕ቯᓟㅌⷺ⠢ᑼߩዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߦ㑐ߒߡ㧘੍஻⊛

ߦផ▚ߐࠇߚዊဳ࠲࡯ࡏࠫࠚ࠶࠻ࠛࡦࠫࡦߩផജߣᲧផജߩᕈ⢻࠺࡯࠲߅ࠃ߮㘑ᵢ⹜㛎ߦࠃߞߡ ᓧࠄࠇߚⓨജ․ᕈ࠺࡯࠲ߦၮߠߊ㘧ⴕ⚻〝⸃ᨆࠍታᣉߒ㧘หᯏ૕ࠍ↪޿ߚ㘧ⴕታ㛎ߩᚑ┙ᕈߩᬌ

⸛ࠍⴕߞߚ㧚ߘߩ⚿ᨐ㧘੹࿁ᗐቯߒߚ࿕ቯᓟㅌⷺ⠢ᑼߩᯏ૕ߪ㧘ㄆ߁ߓߡ⋡ᮡ㘧ⴕࡑ࠶ࡂᢙ

1.4

ߦ೔㆐ߒᓧࠆടㅦ㘧ⴕᕈ⢻ࠍ᦭ߔࠆ߽ߩߩ㧘ߘߩ߹߹ߩ઀᭽ߢߪߘߩᓟߩ኿႐߳ߩᏫㆶ㘧ⴕࡒ࠶

࡚ࠪࡦߩ㆐ᚑߪ࿎㔍ߢ޽ࠆߎߣ߇੍᷹ߐࠇߚ㧚ߎࠇࠄߩᬌ⸛⚿ᨐࠃࠅ㧘ዊဳ⿥㖸ㅦήੱ㘧ⴕᯏࠍ

↪޿ߚ㘧ⴕታ㛎ߩታ⃻ᕈࠍ㜞߼ࠆߚ߼ߦߪ㧘㘧ⴕਛߩΆᢱᶖ⾌㊂ࠍシᷫߔࠆߚ߼ߦ㧘㘧ⴕᤨ㧔․

ߦㆫ࡮⿥㖸ㅦၞ㧕ߩ᛫ജࠍᄢ᏷ߦૐᷫߐߖࠆࠃ߁ߥኻ╷ࠍ⻠ߓࠆߎߣ߇ᦸ߹ࠇࠆ㧚

ෳ⠨ᢥ₂

[1]

K. Mizobata, R. Minato, N. Tanatsugu, H. Kimura, T. Himeno, H. Kobayashi, T. Kojima, S. Aso, Y. Tani, T. Arai,

“Development Plan of a Small-scale Supersonic Flight Experiment Vehicle in Cooperation between Universities”, The 25th International Symposium on Space Technology and Science, ISTS2006-g-20, June 4-11, 2006, Kanazawa, Japan.

[2]

R. Minato, I. Tokura, N. Tanatsugu, T. Himeno, T. Kojima, H. Kobayashi, “Preliminary Design of a Small-scale Turbojet Engine for a Supersonic Flight Experiment Vehicle”, The 25th International Symposium on Space Technology and Science, ISTS2006-g-22, June 4-11, 2006, Kanazawa, Japan.

[3]

Daniel P. Raymer, “Aircraft Design: A Conceptual Approach, Third Edition”, AIAA Education Series, pp. 467-480, 1999.

[4]

H. Kimura, S. Hada, K. Mizobata, R. Minato, N. Tanatsugu, “Flight Trajectory Analysis of a Small-scale Supersonic Flight Experiment Vehicle”, 25th International Symposium on Space Technology and Science, ISTS2006-g-21, June 4-11, 2006, Kanazawa, Japan.

[5]

ᷰㇱജ㧘ฬข੫㧘ዊ࿖ജ⋙ୃ㧘 ̌FORTRAN77 ߦࠃࠆᢙ୯⸘▚࠰ࡈ࠻࠙ࠚࠕ̍ 㧘ਣༀ㧘1989㧚

ᧄ⎇ⓥ䈮㑐䈜䉎⊒⴫⺰ᢥ╬㩷

[1]

Ḵ┵৻⑲㧘Ḋ੫ੑ㇢㧘᫜ᰴਗ਼ᒄ㧘ᧁ᧛ඳᐘ㧘ᆢ㊁ᱞᵗ㧘ዊᨋᒄ᣿㧘ዊፉቁਯ㧘㤗↢⨃㧘⼱ᵏኡ㧘ᣂ੗㓉᥊㧘

̌ᄢቇㅪ៤ߦࠃࠆዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩ㐿⊒᭴ᗐ̍ 㧘╙

49

࿁ቝቮ⑼ቇᛛⴚㅪว⻠Ṷળ㧘

3E05㧘ᐢፉ㧘2005

ᐕ

11

᦬㧚

[2]

ᧁ᧛ඳᐘ㧘⠀↰ዏᄥ㧘Ḵ┵৻⑲㧘Ḋ੫ੑ㇢㧘᫜ᰴਗ਼ᒄ㧘 ̌ዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩ㘧ⴕ⚻〝⸃ᨆ̍ 㧘╙

49

࿁ ቝቮ⑼ቇᛛⴚㅪว⻠Ṷળ㧘3E08㧘ᐢፉ㧘2005 ᐕ

11

᦬㧚

[3]

Ḵ┵৻⑲㧘Ḋ੫ੑ㇢㧘᫜ᰴਗ਼ᒄ㧘ᧁ᧛ඳᐘ㧘ᆢ㊁ᱞᵗ㧘ዊᨋᒄ᣿㧘ዊፉቁਯ㧘㤗↢⨃㧘⼱ᵏኡ㧘ᣂ੗㓉᥊㧘

̌ᄢቇㅪ៤ߦࠃࠆዊဳ⿥㖸ㅦήੱ㘧ⴕᯏߩ㐿⊒᭴ᗐ̍ 㧘╙

3

࿁

HASTIC

ቇⴚ⻠Ṷળ㧘ᧅᏻ㧘2006 ᐕ

3

᦬㧚

[4]

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HASTIC

ቇⴚ⻠Ṷળ㧘ᧅᏻ㧘2006 ᐕ

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[5]

K. Mizobata, R. Minato, N. Tanatsugu, H. Kimura, T. Himeno, H. Kobayashi, T. Kojima, S. Aso, Y. Tani, T. Arai,

“Development Plan of a Small-scale Supersonic Flight Experiment Vehicle in Cooperation between Universities”, 25th International Symposium on Space Technology and Science, 2006-g-20, June 4-11, 2006, Kanazawa, Japan.

[6]

H. Kimura, S. Hada, K. Mizobata, R. Minato, N. Tanatsugu, “Flight Trajectory Analysis of a Small-scale Supersonic Flight Experiment Vehicle”, 25th International Symposium on Space Technology and Science, 2006-g-21, June 4-11, 2006, Kanazawa, Japan.

[7]

K. Mizobata, R. Minato, N. Tanatsugu, H. Kimura, H. Sugiyama, T. Saito, I. Tokura, S. Komazaki, T. Himeno, H.

72

Kobayashi, T. Kojima, S. Aso, Y. Tani, T. Arai, “Development Study on a Small-scale Supersonic Flight Experiment Vehicle with Jet Propulsion in Cooperation between Universities”, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, November 6-9, 2006, Canberra, Australia.